department of aerospace engineering b. tech in aerospace

Department of Aerospace Engineering

B. Tech in Aerospace Engineering

Program Educational Objectives

PEO1 : Graduates will have a successful professional career in the field of aerospace

engineering.

PEO2: Graduates will be able to pursue higher education and research.

PEO3: Graduates will have the ability to work independently as well as in a team with

professional ethics.

Program Specific Objectives

PSO1: Graduates will possess skills in design, development and testing of structures and

systems for aerospace vehicles.

PSO2: Graduates will become professionally competent to take up real time projects through

aerospace industries.

PSO3: Graduates will become globally competitive by pursuing research in multidisciplinary

areas

Course Outcomes (COs)

B.Tech in Aerospace Engineering 2019-20 batch

Semester Course Code

Course Name Course Outcomes (COs)

I 14MA11 Engineering Mathematics-1

CO1 : Employ physical/chemical laws to model the engineering dynamical systems

CO2 : Determine the solution of first and higher order ordinary differential equations

CO3 : Apply Laplace Transforms to solve ordinary differential equations

CO4 : Analyze the system of differential equations with the help of Eigen values and Eigen

14CH12 Engineering Chemistry

CO1 : Able to understand the reaction mechanisms involved in batteries, polymers and fuel combustion

CO2 :Apply their knowledge to solve energy crisis, knocking in IC engine to protect environment

CO3 :Analyze the replacement of conventional materials for domestic and industrial applications

CO4 :Able to determine fluoride nitrate, sulphate, COD, BOD of water

CO5 :Understand the controlling measures taken to control water pollution and corrosion

14EC13 Basic Electronics CO1 :Understand the working of basic electronic components

CO2 :Comprehend the operation of analog and digital circuits.

CO3 :Analyze the working of simple electronic systems.

CO4 :Design small functional building blocks of electronic system

14ME14 Mechanical Engineering Systems

CO1 :Explain the working principles of Hydraulic and Steam turbines

CO2 :Understand the concepts of machine tool operations and different manufacturing process

CO3 :Discuss the basic concepts of Refrigeration and working of IC Engines.

CO4 :Understand the working principles of various power transmission elements

14CS15 Problem Solving Through Programming

CO1 :Understand the components of computing systems, Develop algorithms for mathematical and scientific problems

CO2 :Choose data types and structures to solve mathematical and scientific problem

CO3 :Develop modular programs using control structures

CO4 :Write programs to solve real world problems using programming features

14EG16 English CO1 :Explore new ideas in areas like presentations, group discussions and conversations

CO2 :Transform their pronunciation of English with basic understanding of phonetics

CO3 :Express fluently in flawless English with proper understanding of grammar and syntax

CO4 :Develop command in their language which would build their confidence

CO5 :Identify the salient features of literary texts to produce creative thinking and imaginative writing

14CHL17 Engineering Chemistry Lab

CO1 :Analyze the physical principle involved in the various instruments, also relate the principle to new application

CO2 :Perform different types of titrations in volumetric analysis

CO3 :Exhibit skills in performing experiments based on theoretical fundamentals

14CSL18 Problem Solving Through Programming Lab

CO1 :Read, understand and trace the execution of programs written in C language.

CO2 :Write the C code for a given algorithm.

CO3 :Implement Programs with pointers and arrays, perform pointer arithmetic, and use the pre-processor

CO4 :Write programs that perform operations using derived data types.

II 14MA21 Engineering Mathematics – II

CO1 : Analyze the nature of the data through graphical representations

CO2 :Apply the basic concepts of probability, random variables and its distributions

CO3 :Construct a specific relation for the given bi-variate data using principle of least squares

CO4 :Demonstrate the knowledge of large and small sample distributions in testing

14PH22 Engineering Physics

CO1 :Understand the role of physics in Engineering field

CO2 :Analyze the applications of physics for engineering problems

CO3 :Demonstrate the problem solving ability to identify the solutions

CO4 :Construct the quantum model to explain the behaviour of a system at microscopic level

14EE23 Basics of Electrical Engineering

CO1 :Analyze the AC and DC circuits.

CO2 :Demonstrate the ability to investigate various techniques of earthing & control of lamps

CO3 :Demonstrate the working condition, concepts of Rotating machines and transformers

CO4 :Distinguish between conventional and non- conventional sources & their applications

CO5 :Explain the measurement of power & improvement of Power factor in electrical circuits

14CE24 Basics of Civil Engineering

CO1 :Understand basics of Civil Eng. Building & Public Sewer systems

CO2 :Compute the force system & their effects on Rigid bodies

CO3 :Compute centroid of plain figures, moment of inertia

CO4 :Compute moment of inertia

14ED25 Engineering Drawing

CO1 :Understand the principles of orthographic projections and projection of points in all quadrants.

CO2 :Draw the basic views related to projection of straight lines and planes in first quadrant.

CO3 :Sketch the projections of simple solids like prisms, pyramids, cylinder and cone.

CO4 :Practice the sectional views of solids like cube, prisms, pyramids, cylinders & cones and extend its lateral surfaces.

CO5 :Sketch the isometric projection of simple solids, truncated prisms, pyramids, cone and cylinders .

CO5 :Generate orthographic and isometric views through CAD software

14EWL26 Engineering Workshop

CO1 :Understand the basic concepts of various manufacturing methods.

CO2 :Demonstrate the basic concepts of CNC machining and additive manufacturing process.

CO3 :Produce different joints in fitting.

CO4 :Prepare the different joints in roofs, doors, windows and furniture.

CO5 :Understand the concepts of moulding and casting process.

CO6 :Perform the various welding processes and know about its applications.

14PHL27 Engineering Physics Lab

CO1 :Show the working knowledge of optical, mechanical, electrical and electronics experiments

CO4 :Understand the procedure to conduct the experiments

CO3 :Conduct experiments and correlate with the standard values

III 14MA31 ENGINEERING MATHEMATICS - III

CO1: Develop Fourier series for different types of functions, define and determine Fourier Transform and define Z transform and obtain the solution of difference equations.

CO2: Apply least square method to fit various curves for the given data and interpret the relation.

CO3: Formulate numerical solution of algebraic, transcendental and simultaneous linear equations. Describe and implement the various

numerical methods for Interpolation, differentiation using finite differences. Describe and implement the various numerical methods for the solution of PDE.

CO4: Derive and obtain the solution of wave, heat equation and boundary value problems.

14AE32 MEASUREMENTS AND INSTRUMENTATION FOR AEROSPACE

CO1: Identify the instruments and devices used in the aircraft systems

CO2: Explain the working principles of air data and gyro instruments and its applications

CO3: Explain and Evaluate different parameters used for the engine and sensors used for measurement

CO4: Explain and Evaluate the operation of Flight data recording systems used in Air vehicles

14AE33 AEROSPACE VEHICLES AND SYSTEMS

CO1: Summarize the basics of aircraft and the origins of aircraft designs

CO2: Identify the components of aircraft systems and the aerospace environment

CO3: Classify and understand different aircraft systems, aircraft structures and their effects

CO4: Describe the basics of space dynamics and rocket propulsion

14AE34 FLUID MECHANICS CO1: Identify the fluid characteristics and behavior

CO2: Solve problems in fluid statics

CO3: Apply the laws of motion to fluid flow

CO4: Apply scale effects in moving fluid to fluid flow problems.

14AE35 THERMODYNAMICS CO1: Explain the concepts such as conservation of mass, conservation of energy, work interaction, heat transfer and first law of thermodynamics

CO2: Apply the concept of second law to design simple systems and analyse related problems.

CO3: Analyze the performance of gas and vapor power cycles and identify methods to improve thermodynamic performance

CO4: Demonstrate the importance of phase change diagrams of various pure substances

14AE36 ENGINEERING MECHANICS

CO1: Select appropriate materials for aerospace structures

CO2: Design various aircraft structural components

CO3: Identify the design criteria for maximum stresses and / or maximum displacements

CO4: Use appropriate stress-strain relations for variety of 1D and 2D aircraft structures

14AEL37 MEASUREMENTS AND INSTRUMENTATION LAB

CO1: Design and understand the operation of navigational instrument

CO2: Calibrate a thermocouple and RTD

CO3: Determine the characteristics of potentiometer and strain guage.

CO4: Understand the operation of MEMS based instruments

14AEL38 FLUID MECHANICS LAB

CO1: Calculate coefficient of discharge for different flow meters

CO2: Measure fluid pressure in different equipment’s and relate it to the discharge and flow velocities

CO3: Compare the results of analytical models introduced in lecture to the actual behavior of real fluid flows and draw correct and sustainable conclusions

CO4: Demonstrate the ability to write clear lab reports with good understanding of concepts and their applications in the laboratory.

IV 14MA41 ENGINEERING MATHEMATICS - IV

CO1:Analyze the nature of the data through graphical representations

CO2:Apply the basic concepts of probability, random variables and its distributions

CO3:Construct a specific relation for the given bi-variate data using principle of least squares

CO4:Demonstrate the knowledge of large and small sample distributions in testing

14AE43 MACHINE DRAWING

CO1: Identify the national and international standards pertaining to machine drawing.

CO2: Apply limits and tolerances to assemblies and choose appropriate fits.

CO3: Recognize machining and surface finish symbols.

CO4: Illustrate various machine components through drawings.

14AE44 AERODYNAMICS-I CO1: Explain different types of flows

governing equations and elementary flow characteristics

CO2: Use and apply conformal transformation and thin airfoil models for predicting forces

CO3: Describe incompressible flow over bodies and effect of viscosity on flows.

CO4: Compute and estimate the solution of unsteady aerodynamic problems.

14AE45 AEROSPACE STRUCTURES-I

CO1: Perform analysis, and interpret results of simple aircraft structural elements in the form of beams, frames or truss configurations.

CO2: Demonstrate special aeronautical features like unsymmetrical bending. Shear center and shear flow concepts.

CO3: Idealize a real aeronautical structure in an analytically or a computationally suitable form using alternate approximate methods and mathematical tools like Matrix methods.

CO4: Analyse simplified indeterminate problems applicable to aircraft structures.

14AE46 ENGINEERING MATERIALS AND MANUFACTURING PROCESSES

CO1: Outline the basics of materials, its properties and potential applications in different industry sectors

CO2: Compare different materials and fabrication processes

CO3: Explain the process, equipment and tools used and understanding the process controlling parameters.

CO4: Design and fabricate simple parts and systems through different techniques

14AEL47 AEROSPACE STRUCTURES LAB

CO1: Calibrate and measure the dimensions using various instruments

CO2: Verify the concepts of Strength of Materials and Aircraft Structures.

CO3: Determine stresses and strains by fringe patterns.

CO4: Assess critical loads and mode shapes.

14AEL48 MACHINE SHOP AND PRECISION ENGINEERING LAB

CO1: Prepare process plan for the component given in drawing

CO2: Select of proper tools and work materials and Process planning

CO3: Select of cutting parameters for different machining processes

CO4: Use instruments to measure the dimensions and features on the finished component and to check accuracy and surface finish

V 14AE51 PROPULSION-I CO1: Explain the basic aerothermodynamic principles of aircraft engine components.

CO2: Interpret various performance parameters of aircraft engines.

CO3: Solve, analyze and interpret the basic laws of thermodynamics to engines.

CO4: Recommend selection of propulsion systems for aircraft propulsion.

14AE52 AERODYNAMICS-II CO1: Explain the basics physics behind the governing equations to solve the flow field problems and flow models.

CO2: Apply the principles of quasi one dimensional compressible supersonic flow for determining the performance of the nozzle.

CO3: Apply the normal shock and oblique shock relations for calculating aerodynamic properties for a supersonic flow

CO4: Use the compressible flow equations to estimate the lift and drag coefficient of an airfoil.

14AE53 AIRCRAFT STRUCTURES-II

CO1: Design variety of thin walled structures based on buckling strength.

CO2: Design beam columns under bending and axial loads.

CO3: Analyse aircraft structures under combined loadings.

CO4: Analyse multicell boxes under combined bending, torsion and inplane loads.

14AE54 INTRODUCTION TO SPACE TECHNOLOGY

CO1: Apply the physical laws for the spacecraft orbital movement.

CO2: Describe the solar systems and space environment.

CO3: Apply the stability and spacecraft system design considerations.

CO4: Apply the remote sensing and navigation techniques to satellites systems

14AE55 HEAT AND MASS TRANSFER

CO1: Describe the basic concepts of the different modes of heat transfer

CO2: Explain the physics of conduction, convection and radiation heat transfer.

CO3: Apply the principle of energy-conservation to formulate appropriate mathematical models and choose suitable boundary conditions.

CO4: Solve heat transfer problems in physical systems.

14AE56 COMPOSITE MATERIALS

CO1: Understand properties and applications of materials in aircraft structures and space structures

CO2: Select different types and forms of raw materials used for fabrication and fabrication procedures to make different components and structures

CO3: Identify critical properties and applications of PMCs, MMCs and Carbon-Carbon composites used in aerospace structures and engines

CO4: Describe NDT techniques and their applications in composite structures

14DM57T67 DISASTER MITIGATION

CO1: Discuss about landslide

CO2:Discuss about cyclones protecting engineering structure

CO3:Discuss about Safeguarding during earthquake.

CO4:Construct earthquake resistance structures

14AEL58 AERODYNAMICS LAB

CO1: Describe uses and functioning of wind tunnel equipment

CO2: Measure basic test section flow parameters

CO3: Use measurement data to derive desired results.

CO4: Explain the aerodynamic concepts.

VI 14AE61 AEROSPACE DESIGN I

CO1: Analyze the types of power plants based on their SFC, thrust and efficiency.

CO2: Identify information requirements and critically appraise sources of data and analysis for aircraft design and evaluation.

CO3: Compile and Compute Wing loading, Thrust loading, Performance related data and V-n Diagram

CO4: Estimate the stability characteristics and Design characteristics.

14AE62 FLIGHT

MECHANICS CO1: Predict aircraft performance based on aerodynamic properties and aircraft propulsion systems.

CO2: Employ the equations of motion of an aircraft

CO3: Explain aircraft stability characteristics.

CO4: Identify various aircraft control systems and their operation.

14AE63 PROPULSION - II CO1: Explain the working principles of propulsion systems.

CO2: Apply the principle of energy-conservation to formulate appropriate mathematical models and choose suitable boundary conditions

CO3: Analyze the basic performance parameters of propulsion systems.

CO4: Solve problems on design and performance of propulsion systems.

14AE64 INTRODUCTION TO FINITE ELEMENT METHODS

CO1: Idealize various aircraft structural components

CO2: Apply discretization methods systematically to aircraft components in parts

CO3: Perform various types of analysis for aircraft structural components

CO4: Discuss Post-processing and validation of analysis results

14AE65 FRACTURE MECHANICS

CO1: Compute fracture parameter by LEFM Approach (Griffith’s and Irwin’s approach).

CO2: Compute fracture parameters by EPFM approach (CTOD & J-Integral methodology)

CO3: Describe structures under fatigue loads.

CO4: Use NDT technique for failure analysis and estimation of fracture parameters for metallic and composite structures

14AE662 OPERATION RESEARCH (elective Grp 1)

CO1: Understand phases of an Operational research study and formulate linear programming model for real time problems.

CO2: Apply Graphical method, Simplex algorithm, duality theory and revised simplex algorithm to solve linear programming problems.

CO3: Design and solve transportation and Assignment Models using quantitative techniques.

CO4: Understand and apply critical path analysis and programming

evaluation production and review techniques for timely project scheduling and completion.

CO5: Understand fundamental concepts of game theory and queuing theory.

14AE68 PROPULSION LAB CO1: Estimate and analyze heat transfer coefficient for forced convection over a flat plate and natural convection over an airfoil.

CO2: Calculate the performance of a twin blade propeller.

CO3: Measure the pressure and velocity distribution in a convergent nozzle.

CO4: Determine the growth rate of a free jet by finding the velocity profiles at different locations.

CO5: Predict the pressure distribution on the blade surface of a turbine in cascade wind tunnel.

VII 14AE71 AEROSPACE CONTROL SYSTEMS

CO1: Differentiate types of control systems and develop mathematical model of physical systems

CO2: Analyze a linear physical system for transient and steady responses and assess its stability, using classical control theory methods and extend the same to engineering problems.

CO3: Formulate solutions using basic design methods for solving control problems to meet the desired specifications.

CO4: Explain the concepts of state space based modern control theory and use of MATLAB to solve simple problems.

14AE72 AEROSPACE AVIONICS

CO1: Explain the basics of aircraft navigation systems.

CO2: Compare the different radars and bus systems used in aerospace.

CO3: Outline the working of navigation instruments and systems.

CO4: Apply the inertial navigation systems for aerospace.

14AE73 VIBRATIONS OF ELASTIC SYSTEMS

CO1: Handle numerical analysis and evaluation of single and multiple degrees of freedom vibrating bodies.

CO2: Conduct experimental testing using machinery employed in industry.

CO3: Analyse Vibration measuring instruments and their usage.

CO4: Apply the theories to modern machineries, automobiles, aerofoil sections and landing gears.

14AE74 AEROSPACE DESIGN II

CO1: Make layouts for payloads and systems and estimate various loads acting on aircraft.

CO2: Create preliminary structural design using aerodynamic load, and limit loads.

CO3: Estimate sizing and weight to calculate stresses, strains and displacements of critical structures, while subjected to allowable, limit and ultimate load.

CO4: Discuss trends in design, manufacturing and testing in aerospace industry.

14AE751 COMPUTATIONAL FLUID DYNAMICS & AERODYNAMICS

CO1: Use the various PDEs and solution algorithms for various flow problems.

CO2: Compare turbulence modeling to solve complex engineering problems.

CO3: Apply the numerical skill and discretization skill to analyze the solutions for various flow fields

CO4: Apply linear equation system to solve simple and complex problems

14AEP77 PROJECT PHASE - I CO1:Apply knowledge to identify, gather information to analyze and formulate the problem definition for project through detailed investigation.

CO2:Implement and demonstrate the defined project using appropriate tools

CO3:Recommend sustainable solution/system for the betterment of the society, with scope for enhancement and continue life-long learning.

CO4:Defend the project through effective presentation with professional ethics as an individual or a member of a team

VIII 14AE81 AIRCRAFT SYSTEMS

CO1: Identify aircraft system requirements important to the industry

CO2: Summarze the impact of aerospace systems in a global and societal context

CO3: Use the techniques, skills and modern engineering tools necessary for engineering practice

CO4: Apply aerospace science and engineering to aerospace vehicle design

14AE82 ENGINEERING

MANAGEMENT AND ETHICS

CO1: Identify, formulate and solve problems to engineering management and ethics related issue

CO2: Identify and understand the various engineering ethical related issues and resolve it

CO3: Understand and effectively communicate the fundamentals of decision making

CO4: Act as a good leader to lead society in an ethical way.

14AE83 SEMINAR CO1: Gather information to analyze and formulate the problem definition for a seminar.

CO2: Analyse the defined seminar using appropriate tools.

CO3: Discuss the seminar topic with current aerospace engineering techniques.

CO4: Defend the seminar through effective presentation with professional ethics.

14AEP84 PROJECT WORK CO1:Apply knowledge to identify, gather information to analyze and formulate the problem definition for project through detailed investigation.

CO2: Implement and demonstrate the defined project using appropriate tools

CO3:Recommend sustainable solution/system for the betterment of the society, with scope for enhancement and continue life-long learning.

CO4:Defend the project through effective presentation with professional ethics as an individual or a member of a team

B.Tech in Aeronautical Engineering



engineering.

PEO2: Graduates will be able to pursue higher education and research.




PSO1: Graduates will possess essential skills in design and engineering analysis of

aerospace systems and vehicles.

PSO2: Graduates will be able to execute projects in aerospace industries.

PSO3: Graduates will be able to carry out research in multidisciplinary areas.


B.Tech in Aeronautical Engineering 2019-20 batch

Semester

Course Code


III 18BS3MA01

Mathematics for Aeronautical Engineering

CO1 : Employ physical/chemical laws to model the engineering dynamical systems

CO2 : Determine the solution of first and higher order ordinary differential equations

CO3 : Apply Laplace Transforms to solve ordinary differential equations

CO4 : Analyze the system of differential equations with the help of Eigen values and Eigen

CO5 : Apply the basic concepts of probability, random variables and its distributions

CO6 : Construct a specific relation for the given bi-variate data using principle of least squares

18HSS03 Economics for Engineers

CO1: To identify and explain economic concepts and theories related to the behavior of economic agents, markets, industry and firm structures, legal institutions, social norms, and government policies.

CO2: To demonstrate an awareness of the role in the global economics environment

CO3: To analyse business and managerial economic decisions

CO4: To evaluate the consequences of economic activities and institutions for individual and social welfare.

CO5: To demonstrate an awareness of socio-economic policies of the central banks and central governments

CO6: To evaluate current economic scenarios

18AN32 Engineering Materials & Manufacturing Processes

CO1 : Illustrate basics of materials, its properties and potential applications in Aircraft and Aerospace.

CO2 : Completely understand of casting and special casting processes and to application in industries

CO3 : Demonstrate sheet metal fabrication relating to aircraft and space craft applications

CO4 : Exposure to welding processes preferably used in aircraft and space craft applications

CO5 : Plan for manufacturing simple components used in aircraft applications by forging and rolling operations

CO6 : Outline the requirements for drawing and extrusion processes with respect to fabrication of different components like hollow and solid cross sections

18AS33 Fluid Mechanics CO1 : Identify the fluid characteristics and behavior and demonstrate the application to problems in fluid properties.

CO2 : Explain and apply the concepts and problems in fluid statics.

CO3 : Use of the laws of motion to solve and examine the fluid motion.

CO4 : Use of scale effects in moving fluid to simplify problems. Employ the simplified viscous flow solutions to fluid flow.

CO5 : Explain the basic terminologies and use the modeling concepts to solve problems.

CO6 : Explain the effect of boundary layer to fluid flows and compute boundary layer parameters.

18AS34 Introduction to Aerospace Vehicles and Systems

CO1 : Describe the fundamentals of airplane and helicopters along with its operating principle.

CO2 : Explain the operating principle of power plants in aviation industry

CO3 : Identify the structural components of aircraft and describe the materials used in the field of aviation.

CO4 : Classify different types of airplane Hydraulic, Pneumatic, Fuel, Electrical & Communication systems and Flight Control Systems

CO5 :Classify the landing gear components and describe about Flight envelope

CO6 : Describe the basics of space dynamics and rocket propulsion

18AS35 Engineering Mechanics

CO1 : Identify the physical phenomena & understand the importance of mechanical

properties of rigid and deformable bodies in aircraft structures

CO2 : Apply the stress – strain relations for variety of aircraft structures subjected to various loading conditions

CO3 : Analyze beams for effect of shear and bending for design of beams.

CO4 : Analyze the shafts and beams including deflection as design criteria for structural members.

CO5 : Estimate the design factors for shafts and springs for the given data.

CO6 : Apply energy theorems for structural analysis

18AN32L Machine shop and precession engineering lab

CO1 : Describe the industry lay-out and to draft a layout

CO2 : Select cutting parameters for different machining processes

CO3 : Perform various precision measurement techniques

CO4 : Perform various operations using lath

CO5 : Perform various other manufacturing processes such as milling, shaping, drilling etc.,

CO6 : Select a machining process and proper tools appropriate for the work material or the requirement

18AS33L FLUID MECHANICS LAB

CO1 : Measure pressure using Vernier Calipers for finding coefficient of discharge for V-Notch

CO2 : Measure pressure using U-tube Manometer for different flow measuring devices.

CO3 : Compare the coefficient of discharge between Orifice meter, Nozzle meter and venturimeter to find the accurate flow meter.

CO4 : Calculate head loss due to friction in turbulent flow

CO5 : Compare the minor losses due to change of section, valve, bend or any other interruption

CO6 : Determine the force exerted by the jet on vanes

IV 18AS41 Thermal Science

CO1 : Explain and demonstrate the concepts of energy and energy interactions.

CO2 : Identify the assumptions that are to be made for an engineering design.

CO3 : Apply the laws of thermodynamics to diverse engineering problems.

CO4 : Analyze and decide the feasibility of design variables using thermodynamics principles.

CO5 : Develop new ideas to an engineering design satisfying thermodynamics and heat transfer principles.

CO6 : Analyze the combined modes of heat transfer in engineering applications.

18AN42 Aerodynamics CO1 : Illustrate the basic physics behind the different types of flow, governing equations.

CO2 : Use the basic flow models, conformal transformation and thin airfoil models for predicting forces.

CO3 : Examine the 2D or 3D flow models in aerodynamics for lift and drag computations.

CO4 : Identify the principles of one dimensional compressible supersonic flow for determining the performance of the nozzle.

CO5 : Use the normal shock and oblique shock relations for calculating aerodynamic properties for a supersonic flow.

CO6 : Use the compressible flow equations to estimate the lift and drag coefficient of an airfoil.

18AN43 Measurements and Instrumentation for Aerospace

CO1 : Compare the basic Instruments used in Aircraft.

CO2 : Distinguish various display devices used in Aircraft

CO3 : Explain the principle of operation of Air Data Instruments and Gyroscopic instruments used in Aircraft.

CO4 : Explain the operation of various engine instruments and pressure instruments used in Aircrafts

CO5 : Describe the operation of the fuel Instruments used in aircrafts

CO6 : Discuss the functioning of flight data recorders and application of instruments.

18AS44 Data Structures using C

CO1 : Understand the concepts of data structure, algorithms and ADT.

CO2 : Apply linear and non-linear data structures in real world problems.

CO3 : Demonstrate Tree and Hashing to handle the data efficiently.

CO4 : Analyze data structures and algorithms to solve real world problems.

CO5 : Evaluate searching and sorting algorithms.

CO6 : Design the data representation using graph technique

18AN45 CAD Lab using CATIA v5

CO1 : Provide skills in modern tools involved for modeling in Industry.

CO2 : Identify the national and international design standards pertaining to professional drawing.

CO3 : Apply limits and tolerances to assemblies and choose appropriate fixtures and joints

CO4 : Recognize location of critical components location in an assembly sketch.

CO5 : Introduce new design ideas for reducing of size and weight.

CO6 : Apply the different standards in drafting the designed model.

18HSS04 Business Communication and Presentation Skills

CO1 : To distinguish among various levels of organizational communication and communication barriers

CO2 : To participate in an online learning environment successfully by developing the implication-based understanding of paraphrasing, deciphering instructions, interpreting guidelines, discussion boards & Referencing Styles

CO3 : To demonstrate his/her ability to write error free while making an optimum use of correct business vocabulary and grammar.

CO4 : To draft effective business correspondence with brevity and clarity.

CO5 : To stimulate critical thinking by designing and developing clean and lucid writing skills.

CO6 : To demonstrate verbal and non-verbal communication ability through presentations.

18AN42L AERODYNAMICS LAB

CO1 : Analyze the air flow in a wind tunnel.

CO2 : Experimentally measure the aerodynamic coefficients of an airfoil.

CO3 : Measure the aerodynamic forces using wind tunnel balances.

CO4 : Obtain the boundary layer thickness and velocity profile.

CO5 : Calculate the wake thickness.

CO6 : Conduct flow visualization studies.

18AN43L MEASUREMENTS AND INSTRUMENTATION LAB

CO1 : Measure bearing angle using magnetic compass to understand the use of navigational instruments.

CO2 : Measure temperature using thermocouple and designed RTD circuits.

CO3 : Examine the given signal characteristics using oscilloscope.

CO4 : Determine the target’s speed using RADAR equipment.

CO5 : Measure load using strain gauge and displacement using potentiometer.

CO6 : Measure pressure and acceleration using MEMS sensor

V 18AN51 Aircraft Propulsion

CO1 : Explain the basic aerothermodynamic principles of aircraft engine components.

CO2 : Recognize typical engine design components and their characteristics.

CO3 : Estimate performance parameters of aircraft engines and its components.

CO4 : Solve, analyze and interpret the basic laws of thermodynamics to engines.

CO5 : Match performance criterion for selecting engine component.

CO6 : Recommend selection of propulsion systems for aircraft propulsion.

18AS52 Flight Mechanics-I (Performance)

CO1 : Explain various aerodynamic characteristics and propulsive efficiencies of piston-propeller and jet engines

CO2 : Calculate the performance characteristics like cruise, ascent and descent, turning, range and endurance of an aircraft.

CO3 : Describe aircraft take-off, landing and noise characteristics.

CO4 : Predict aircraft performance based on aerodynamic properties and engine performance.

CO5 : Determine aircraft static stability, control and various mission profiles of different types of aircraft.

CO6 : Outline the concept of aircraft noise and their effects on humans.

18AN53 Aircraft Structures

CO1 : Perform analysis, and interpret results of simple aircraft structural elements in the form of beams and frames.

CO2 : Analyse stable planar and space trusses .

CO3 : Demonstrate special aerospace features like unsymmetrical bending, Shear center and shear flow concepts.

CO4 : Idealize complex aircraft structures for the analysis of determinate problems.

CO5 : Solve indeterminate problems using energy methods.

CO6 : Comprehend stability related behavior of column type structures.

18AN54 Introduction to Helicopters

CO1 : Identify the Parts of Helicopters and Explain their functionality

CO2 : Apply the Momentum theory for Analysis of Helicopter Aerodynamics

CO3 : Apply the Blade Element theory for Analysis of Helicopter Aerodynamics

CO4 : Differentiate the Momentum theory and Blade element theory for Analysis of Helicopter Aerodynamics

CO5 : Calculate the performance parameters in various flight Conditions

CO6 : Describe helicopter rotor dynamics, sources of helicopter vibrations and means of reduction.

18AS55 Matlab with Applications

CO1 : Apply the principle of energy conservation and Fourier’s law to solve one-dimensional heat conduction problems.

CO2 : Analyze both steady and unsteady one-dimensional heat conduction problems by

applying the concepts of thermal resistance and overall heat transfer coefficients

CO3 : Apply numerical methods to solve one-dimensional and two-dimensional heat conduction problems.

CO4 : Analyze heat exchanger problems and solve heat convection problems by applying the basic concepts of conduction and momentum conservation.

CO5 : Apply the concepts of radiation heat transfer to solve combined heat transfer problems.

CO6 : Apply the concepts of mass diffusion and convection to solve mass transfer problems

18AN51L Propulsion Lab CO1 : Estimate and analyze heat transfer coefficient for forced convection over a flat plate and natural convection over an airfoil.

CO2 : Calculate the performance of a twin blade propeller.

CO3 : Measure the pressure and velocity distribution in a convergent nozzle.

CO4 : Determine the growth rate of a free jet by finding the velocity profiles at different locations.

CO5 : Predict the pressure distribution on the blade surface of a turbine in cascade wind tunnel.

CO6 : Determine the speed of premixed flame with mass flow rates.

18AN53L AEROSPACE STRUCTURES LAB-I

CO1 : Differentiate between statically determinate and indeterminate structures.

CO2 : Apply equations of equilibrium to structures and compute the reactions.

CO3 : Determine various unknowns based on Statics through many theorems and concepts.

CO4 : Analyze and draw the influence lines for reactions.

CO5 : Determine stresses and strains by fringe patterns.

CO6 : Assess critical loads and mode shapes.

VI 18AS61 Avionics CO1 : Demonstrate the communication principle to aircraft systems.

CO2 : Compare the different radar systems used in aircraft.

CO3 : Explain the different navigation concepts for aircraft .

CO4 : Compare the navigation systems used in the aircraft.

CO5 : Apply bus architecture to aircraft communication .

CO6 : Implement GPS principles to aerospace applications.

18AN62 Control Systems CO1 : Differentiate the types of control systems.

CO2 : Develop mathematical model for different dynamical systems.

CO3 : Analyze stability of dynamical systems based on the classical control theory.

CO4 : Implement controllers and compensators using PID.

CO5 : Formulate solutions using classical control system design methods for solving control problems to meet the desired specifications.

CO6 : Analyze dynamical system using modern control theory i.e., state space analysis and use of MATLAB to solve simple problems.

18AN63 COMPOSITE MATERIALS

CO1 : Select materials for different aircraft structures under different service conditions.

CO2 : Select different types and forms of raw materials used for fabrication and fabrication procedures to make different components and structures

CO3 : Compare different mechanical properties of polymer matrix and metal matrix composites along with their applications in structures

CO4 : Use ceramic matrix and carbon matrix composites for aircraft engine and space structures

CO5 : Elaborate on high speed aerodynamics, thermal barrier coatings and ablative coatings

CO6 : Describe NDT techniques and inspect composite structure for defect analysis and evaluation

18AS641 Rocket Propulsion

CO1 : Apply the basic principles of rocket propulsion to evaluate performance parameters.

CO2 : Apply the principle of energy-conservation to solve nozzle flow problems.

CO3 : Apply the concepts of combustion to design thrust chambers.

CO4 : Design solid and liquid propulsion systems and analyze their performance.

CO5 : Apply the elements of solid and liquid propulsion systems to cryogenic and hybrid propellant rockets.

CO6 : Solve and analyze multi staging problems.

18AS642 Flight Mechanics-II (Stability and Control)

CO1 : Derive governing equations and linearize them.

CO2 : Predict steady and quasi-steady aerodynamic derivatives

CO3 : Derive open loop transfer function for longitudinal and later-directional motion

CO4 : Study stability characteristics.

CO5 : Apply various aircraft handling qualities and stability augmentation systems.

CO6 : To understand control augmentation and its various types.

18AS651 Introduction to

Fracture Mechanics

CO1 : Outline the fundamentals of fracture through conventional and modern design approaches.

CO2 : Explain fracture based problems by LEFM Approach (Griffith’s and Irwin’s approach).

CO3 : Explain fracture based problems by EPFM approach (CTOD & J-Integral methodology).

CO4 : Relate and solve a Structure under fatigue loads.

CO5 : Distinguish the failure mechanisms in composites.

CO6 : Describe NDT techniques and can justify their applications.

18AS652 Introduction to Finite Element Methods

CO1 : Ability to idealize various aircraft structural components.

CO2 : Apply discretization methods systematically to aircraft components in parts.

CO3 : Acquire the knowledge of writing FEM codes for structural and thermal analysis software packages.

CO4 : Perform various types of analysis for aircraft structural components.

CO5 : Acquire the knowledge of post-processing and validation of the analysis results.

CO6 : Apply software knowledge to solve practical problem.

18AN66L Aerospace Structures Lab-II

CO1 : Calibrate and measure the dimensions using various instruments.

CO2 : Verify the concepts of Strength of Materials and Aircraft Structures.

CO3 : Determine stresses and strains by fringe patterns.

CO4 : Assess critical loads and mode shapes.

CO5 : Explain the mechanics of modern fiber reinforced composites and their fabrication.

CO6 : Evaluate simple mechanical property testing of standard specimens.

18AS67P Flight Lab Course

CO1 : Understand what an aircraft, glider is with hands on experience

CO2 : Importance of aircraft CG and its relevance of movement

CO3 : Calibrate system instrumentation

CO4 : Experience Flight

CO5 : Appreciate theory and practice

CO6 : Conduction of experiments during flight Appreciate and compare various facilities

VII Aerospace Design

CO1 : Outline the basics of aerodynamics, propulsion and structures for the Preliminary design calculations.

CO2 : Identify design requirements and compute weight estimation, fuel load estimation.

CO3 : Compile and Compute Wing loading, Thrust loading, Performance related data and V-n Diagram.

CO4 : Estimate the stress and design margins for all the primary and secondary structural members.

CO5 : Estimate the stability characteristics and Design characteristics of the model developed by using software’s.

CO6 : Identify design and manufacturing tolerances followed in the aerospace industry.

VII Computational Fluid Dynamics

CO1 : Analyze mathematical models for modeling of various flow problems.

CO2 : Classify partial differential equations based on the mathematical and physical properties modeled by them.

CO3 : Analyze and apply finite difference method for solution of partial differential equations governing fluid flow.

CO4 : Analyze and apply finite volume method for for solution of partial differential equations governing fluid flow.

CO5 : Analyze and apply time discretization schemes for fluid flow problems.

CO6 : Apply numerical methods to solve incompressible and compressible flow problems

VII UAV Systems CO1 : Describe the historical evolution of Unmanned Aerial Vehicles (UAVs), their applications and regulations related to UAVs

CO2 : Explain the terminology specific to UAVs

CO3 : Apply the concepts of Aerodynamics, Propulsion, Structures and Systems to UAVs

CO4 : Analyze basic Fixed Wing and Rotary Wing UAVs design problems

CO5 : Categorize UAV payloads and sizing based on mission requirements

CO6 : Analyze Mission Plans for UAVs

VII Aircraft Systems CO1 : Identify aircraft system requirements important to the industry

CO2 : Summarize the impact of aerospace systems in a global and societal context

CO3 : Ability to use the techniques, skills and modern engineering tools necessary for engineering practice

CO4 : Apply aerospace science and engineering to aerospace vehicle design

CO5 : Demonstrate professional and ethical responsibility

CO6 : Engage in life-long learning.

VII Air Traffic Management

CO1 : Describe the general principles and theories of operation of the air traffic control system.

CO2 : Outline Air Traffic Services around the globe.

CO3 : Explain the procedures used in radar and non-radar air traffic control.

CO4 : Explain international air traffic control.

CO5 : Discuss future enhancements to the national airspace system.

CO6 : Interpret Aviation 192 (Instrument Flight) with a sound grasp of instrument flight procedures.

VII VIBRATIONS OF ELASTIC SYSTEMS

CO1 : Analyze vibration of multi-degree-of-freedom-discrete systems

CO2 : Analyze vibration of multi-degree-of-freedom-discrete systems

CO3 : Analyze vibration of continuous systems

CO4 : Analyze vibrations of nonlinear systems and random vibrations

CO5 : Learn the experimental technique to solve complex engineering vibration problems

CO6 : Apply knowledge of vibration to solve aeroelastic problems

VII Introduction to FRACTURE MECHANICS

CO1 : Interpret fundamentals of fracture through conventional and modern design approaches.

CO2 : Explain fracture based problems by LEFM Approach (Griffith’s and Irwin’s approach).

CO3 : Explain fracture based problems by EPFM approach (CTOD & J-Integral methodology).

CO4 : Solve a Structure under fatigue loads.

CO5 : Distinguish and infer on failure mechanisms in composites.

CO6 : Describe NDT techniques and can justify about their applications.

VII INTRODUCTION TO MICRO ELECTRO MECHANICAL SYSTEMS

CO1 : Explain the basics of Micro Electro Mechanical Systems(MEMS) and Applications

CO2 : Analyze the scaling laws and its practical use to MEMS

CO3 : Apply the MEMS process for devices processing

CO4 : Explain the polymer MEMS and its application

CO5 : Apply the Semiconductor packaging and testing techniques for MEMS

CO6 : Apply the MEMS for real world application

VII COMPUTATIONAL ANALYSIS LAB

CO1 : Demonstrate various steps involved in performing the structural analysis of aircraft structural components using MSC Patran, Nastran.

CO2 : Apply various boundary conditions, material properties and given loading conditions on MSC patran tool.

CO3 : Become adept at using different meshing techniques on MSC Patran.

CO4 : Interpret the results of analysis by comparing them with theoretical values.

CO5 : Use ANSYS Fluent software for analysis of airfoils, nozzle etc. and other aerospace systems/components

CO6 : Capable of performing different meshes using ANSYS

VIII Introduction to UAV Technologies

CO1 : To understand basic UAV elements

CO2 : Describe the parts and functions of UAV & Indian Aviation regulations of UAV

CO3 : Explain the concepts of Aerodynamics, Propulsion & Structures of Model Aircrafts

CO4 : Describe the working principle and components of UAV

CO5 : Demonstrate the design process of UAV

CO6 : Demonstrate design, fabrication and Flying of UAV

VIII Operation Management

CO1 : Summarize organization objectives and functionss and understand, evaluate & apply issues in services & manufacturing operations.

CO2 : Describe trends and developments in operation management and use them for design of operations systems elements & their modifications.

CO3 : Explain the role and importance of planning and scheduling, hierarchy in planning, Strategic planning, business plan, operations strategy

CO4 : Outline strategic and tactical decision making and Apply and carry out techniques of aggregate planning and master scheduling, operational decision making.

CO5 : Apply forecasting tools and carry out capacity planning, disseminate & use data in all concerned functional areas

CO6 : Explain materials management, Supply chain management, its evolution, objectives, processes and techniques, functions of inventory control, inventory costs and purchase and apply the understanding to manage supply chain elements

VIII Engineering Management and Ethics

CO1 : Comprehend and evaluate the basic principles of the fundamentals of engineering management

CO2 : Identify and apply appropriate management techniques for managing contemporary organizations

CO3 : Demonstrate an understanding of personnel management and motivational theories

CO4 : Distinguish between ethical and non-ethical situations

CO5 : Practice moral judgment in conditions of dilemma

CO6 : Apply risk and safety measures in various engineering fields

VIII Basics of Research and Development

CO1 : Outline the basic concepts of R&D

CO2 : Describe the research process and methodology in R&D

CO3 : Differentiate the types of R&D

CO4 : Explain the research methodology of R&D

CO5 : Summarize the admin and evaluation process of R&D

CO6 : Discuss the future of R&D organizations

M.Tech in Aerospace Engineering - Avionics Specialization


PEO 1: Graduates of the program will be able to lead teams or have a successful

professional career in industry/academia.

PEO 2: Graduates of the program will have the ability to pursue higher studies and

independently carry out research and development work to solve societal problems.

PEO 3: Graduates of the program will have the ability to design and implement solutions in

the area of avionics for rapidly changing technical rquirements and lifelong learning to adapt

to innovation.


PSO 1: Graduates will possess skills in design, development and testing of avionics and

systems for aerospace applications.

PSO 2: Graduates will become professionally competent to take up real time projects

through aerospace industries.

PSO 3: Graduates will become globally competitive by pursuing research in the area of

avionics.


M.Tech in Aerospace Engineering - Avionics Specialization 2019-20 batch

Semester

Course Code


I 18MTMAE101

MATHEMATICS FOR AEROSPACE ENGINEERS

CO1: Solve the matrices, vectors and other lienar equations

CO2: Employ the Fourior series and partial diffrential equations for analyzing circuits and systems in aerospace.

CO3: Apply Lapace transformations and other mathematical equations like power serious , taylor serious for solving problems

CO4: Employ appropriate algebric equations and numerical methods to solve Initial value problems

18MTMCC01

ENGLISH FOR RESEARCH PAPER WRITING

CO 1: To craft persuasive, complex, inquiry-driven arguments dealing with engineering and technology

CO2: To work strategically with complex information in order to generate and support inquiry by reading, analyzing, and synthesizing a diverse range of data

CO3: To compose technical articles for a variety of audiences and contexts, both within and outside the academia

CO 4: To practice writing technical articles as a collaborative process and to develop flexible strategies to deal with giving, receiving, interpreting, and incorporating constructive feedback

18MTADE101

INTRODUCTION TO AEROSPACE VEHICLES

CO1: Summarize the basics of aircraft and the origins of aircraft designs

CO2: Identify the components of aircraft systems and the aerospace environment

CO3: Classify different aircraft systems, aircraft structures and their effects

CO4: Able to understand the basics of space dynamics and rocket propulsion

18MTAVS101

INTRODUCTION TO AVIONIC SYSTEMS

CO1: Apply avionics System for civilion , defence applications and avionics standards

CO2: Employ conventional sensors and MEMS sensors for aerospace appliactionas.

CO3: Choose different bus architure and display systems for aerospace communication.

CO4: Use different supporting systems for aerospace appliactions

18MTAVS102

SOFTWARE ENGINEERING AND DIGITAL SIGNAL PROCESSING

CO1: Discuss the given project in various phases of a lifecycle.

CO2: Choose appropriate process model depending on the user requirements.

CO3: Use the knowledge, techniques, and skills in the development of a software product.

CO4: Discuss architecture and application of digital signal processors

18MTAVS131

PRINCIPLES OF REAL TIME COMPUTING

CO 1:Explain concepts of Real-Time systems and modeling

CO 2:illustrate the characteristics of a real-time system

CO 3:develop document on an architectural design of a real-time system

CO 4:develop and document Task scheduling, resource management, real-time operating systems and fault tolerant applications of Real-Time Systems.

18MTAVS132

DESIGN AND ANALYSIS OF ALGORITHMS

CO 1:Demonstrate a familiarity with major algorithms and data structures.

CO 2:explain important algorithmic design paradigms (divide-and-conquer, greedy method, dynamic-programming and Backtracking) and apply when an algorithmic design situation calls for it.

CO 3:Explain the major graph algorithms and Employ graphs to model engineering problems, when appropriate.

CO 4:analyze Cryptographic Computations, Information Security Algorithms and Protocols

18MTAVS101L

AVIONICS SYSTEMS LAB

CO1: Understand the Mil-STD 1553B Protocol

CO2: Understand the messages for communication between systems

CO3: Understand the data exchanging between the various avionics systems

CO4: Understand the mode code communication for checking the protocol health status

II 18MTAVS201

NAVIGATION AND COMMUNICATION SYSTEMS

CO 1:Compare the navigation systems used in the aircraft.

CO 2:Implement GPS principles and Kalman filter techniques to aerospace applications.

CO 3:Apply the communication networks for aerospace applications

CO 4:Apply the communication systems and antennas for aerospace applications

18MTAVS202

PROBABILITY THEORY

CO1: Introduced to the techniques of developing discrete & continuous

MODELLING AND SIMULATION

probability distributions and its applications.

CO2: Able to describe a random process in terms of its mean and correlation functions.

CO3: Aware with the special processes like Poisson, Renewal processes,and derive the backwards & forwards equation

CO4: Able to specify a given discrete and Markov chain in terms of a transition diagram.

18MTAVS203

SURVEILLANCE SYSTEMS

CO 1:To introduce the basic and advanced radar operation

CO 2:To explain the working of TCAS Unit and TCAS display

CO 3: To understand the functioning of ADSB Unit.

CO 4: To study the recent advances in Surveillance Systems

18MTAVS221

LINEAR ALGEBRA & ITS APPLICATIONS

CO1 : Recognize when linear algebra concepts can be applied to a variety of mathematical and engineering problems

CO 2: Demonstrate the ability to apply numerical methods to solve linear algebra problems with accuracy,precision, and efficiency

CO 3: To gain intuition for core concepts, including: eigenvalues and eigenvectors, singular value decompositions,duality, rank, and determinants

CO 4: Use technology, where appropriate, to enhance and facilitate in solving linear algebraic problems and presenting solutions

18MTAVS222

FLIGHT TEST INSTRUMENTATION AND FLIGHT MANAGEMENT SYSTEMS

CO 1:To introduce the basic concepts of the fight testing and flight-testing requirements

CO 2: To comprehend the principle of operation of Air Data Instruments.

CO 3:To understand the operation of various Engine Instruments and the pressure Instruments used in Aircrafts

CO 4:To study the functionality of FMS and aircraft telemetry systems

18MTAVS231

NUMERICAL METHODS

CO1 : Be aware of the use of numerical methods in modern aerospace and avionics engineering.

CO 2: Derive numerical methods for various mathematical operations and tasks, such as interpolation, differentiation, integration, the solution of

linear and nonlinear equations, and the solution of differential equations.

CO 3: Analyse and evaluate the accuracy of common numerical methods.

CO 4: Apply numerical methods to obtain approximate solutions to mathematical problems.

18MTAVS232

CONTROL SYSTEM ENGINEERING

CO 1:Understand open loop and closed loop control systems, types of control systems and develop mathematical model of physical systems

CO 2:To analyze a linear physical system for transient and steady responses and assess its stability, using classical control theory methods and extend the same to engineering problems.

CO 3:Formulate solutions using basic design methods for solving control problems to meet the desired specifications.

CO 4:Become familiar with concepts of state space based modern control theory and use of MATLAB to solve simple problems.

18MTAVS203L

RADAR LAB CO 1:Uunderstand the operation of basic radar

CO 2:Understand the operation of advanced radar

CO 3:Determine the range and velocity of the distant objects

CO 4:Determine the directivity and gain of antennas and to compare them

18MTAVS204L

NAVIGATION LAB/COMMUNICATION LAB

CO 1:Understand the position fixing using dead reckoning and multiple bearing

CO 2: Measure airspeed using IMU in the wind tunnel and experiment with IMU to sense parameters using dynamic conditions

CO 3:Generate AM and FM waves and study the characteristics

CO 4:Understand the data coding and decoding technique

III 18MTAE301 RESEARCH METHODOLOGY

CO 1:Apply a range of quantitative and / or qualitative research techniques to business and management problems / issues

CO 2:Demonstrate knowledge and understanding of data analysis and interpretation in relation to the research process.

CO 3:Conceptualise the research process.

CO 4:Assess critically the following methods: literature study, case study, structured surveys, interviews, focus groups, participatory approaches, narrative analysis, scenario methodology and basic statistical methods.

18MTAVS301

LANDING AID SYSTEM & AIR TRAFFIC CONTROL SYSTEMS

CO 1:Classify the equipment characteristics and specifications of airport visual landing aids.

CO 2:Determine use cases for aircraft and airport navigation aids using ILS, MLS and satellite based navigation.

CO 3:Explain the concept of airborne warning systems for ground proximity and weather related threats.

CO 4:Apply airborne equipment to counter proximity threats due to air traffic to reduce mid-air collisions.

18MTAES303

SEMINAR CO 1:Gather information to analyze and formulate the problem definition for a seminar.

CO 2:Analyse the defined seminar using appropriate tools.

CO 3:Discuss the seminar topic with current aerospace engineering techniques.

CO 4:Defend the seminar through effective presentation with professional ethics.

18MTAEP304

PROJECT WORK CO 1:Apply knowledge to identify, gather information to analyze and formulate the problem definition for project through detailed investigation.

CO 2:Implement and demonstrate the defined project using appropriate tools

CO 3:Recommend sustainable solution/system for the betterment of the society, with scope for enhancement and continue life-long learning.

CO 4:Defend the project through effective presentation with professional ethics as an individual or a member of a team

18MTAVS321

ADVANCED EMBEDDED SYSTEMS

CO 1:To analyze embedded system architecture and to develop I/O SW

CO 2:To apply the c Progeamme for microcintrolers

CO 3:To identify test requirements for SW on host machine

CO 4:To analyze RTOS scheduling models and OS security issues

18MTAVS322

TOPICS ASSOCIATED

CO1: Apply System requirement analysis methods for decomposition of functions among systems and sub systems

WITH AVIONICS SYSTEMS

CO2: Build message structures using databus concepts and to evolve conceptual avionics system architectures

CO3: Evolve avionics test bench architecture

CO4: Aerospace Navigation and Communication systems

IV 18MTAEP404

PROJECT WORK CO 1:Apply knowledge to identify, gather information to analyze and formulate the problem definition for project through detailed investigation.

CO 2:Implement and demonstrate the defined project using appropriate tools

CO 3:Recommend sustainable solution/system for the betterment of the society, with scope for enhancement and continue life-long learning.

CO 4:Defend the project through effective presentation with professional ethics as an individual or a member of a team

M.Tech in Aerospace Propulsion Technology



propulsion.

PEO2: Graduates will be able to pursue higher education and research in aerospace

propulsion.




PSO1: Graduates will possess skills in design, development and testing of propulsion

systems for aerospace vehicles.

PSO2: Graduates will able to carry out research in multidisciplinary areas.


M.Tech in Aerospace Propulsion Technology 2019-20 batch

Semester Course Code Course Name Course Outcomes (COs)

I 18MTADE101 Introduction to Aerospace Vehicles

CO1 :To explain characteristics of airfoils, use of wind tunnel, basics if airplane stability, and Helicopters CO2: To identify the materials used for aircraft structure and its structural layout CO3: To explain working principles of different types of airbreathing propulsion systems and propulsion in helicopters CO4: To explain major aircraft systems and aircraft navigational aids CO5: To explain forces on a body in a central force field, rocket propulsion, and typical launch vehicle configurations

I 18MTMAE101 MATHEMATICS FOR AEROSPACE ENGINEERS

CO1 : Solve ordinary and partial differential equations using numerical techniques CO2 : Apply principles of matrix algebra to linear transformations. CO3 : Analyze the functions and signals using Fourier series and Fourier transforms CO4 : Apply the concept of Calculus on Complex functions

I 18MTAPT101 Gas Dynamics CO1: Derive and interpret the terms in

governing equations of 3D compressible flow CO2: Apply normal shock relations to calculate pressure loss in practical situations CO3: Calculate pressure distribution on plane surfaces with compression and expansion corners CO4: Explain method of characteristics applied to determine supersonic nozzle contour CO5: To recommend simple measurements required for calculations of compressible flow through ducted components.

I 18MTAPT102 Aircraft Propulsion CO1: Describe the performance parameters and Explain the aerodynamics design-aspects of turbomachinery. CO2: Calculate fatigue safety factor and creep life of gas turbine components. CO3: Identify sources of blade excitation and methods of dealing with them. CO4: Explain the requirement and working of sub-systems

I 18MTADE102 Aerodynamics and Flight Mechanics

CO1 : Modeling of bodies for aerodynamic analysis. CO2 : Exposure to different airfoils, understating the influence of each of geometric parameter of the airfoil on aerodynamic forces & moments. CO3 : Calculation of aircraft performance with specific reference to different speeds, range & endurance. CO4 : Ability to do flight mechanics calculations.

I 18MTAPT131 Aero Engine Performance Evaluation

CO1: Perform analysis of ideal engines CO2: Estimate component performance given the efficiency inputs CO3: Explain basic steps of real engine cycle calculation CO4: Explain steps for calculation for turbofan engine performance CO5: Carry out performance analysis of Turbojet and turbofan engines

I 18MTASD101L Aero-Structures

Lab CO1 : To measure the dimensions of various specimen by Vernier Caliper, Dial Gauge that finds applications in all the experiments. CO2 : To enable the students to understand the various theorems and calculations based on Strength of Materials and Aircraft Structures approach.. CO3 : To study the fringe patterns of Stress and Strain using Photoelastic techniques. CO4 : To understand the concepts of Vibrations and Elastic Stability.

II 18MTADE201 COMPUTATIONAL FLUID DYNAMICS

CO1 : Derive governing equations for fluid flow. Learn various forms of governing equations and their significance. CO2 :Classify partial differential equations and learn the properties. CO3 :Learn different kinds of discretization methods for partial differential equations. CO4 :Identify the conditions to be satisfied by the numerical scheme, consistency, stability and accuracy. CO5 :Develop computer codes for Computational fluid dynamics.

II 18MTAPT201 Heat Transfer and Combustion

CO1: Demonstrate an understanding of the basic concepts of heat transfer. CO2: Apply the concepts of mass, momentum and energy conservation to heat transfer problems. CO3: Formulate the differential equations and boundary conditions to solve convection problems. CO4: Demonstrate an understanding of the basic concepts of combustion. CO5: Analyze the problems of flame stabilization and combustion instability

II 18MTAPT202 Design and Development of Aero-Engine Systems and Testing

CO1: Explain the aerodynamics design-aspects of gas turbine modules CO2: Recommend testing procedures of Gas turbine engines and components CO3: Explain the functions and requirements of secondary systems. CO4: Describe gas turbine engine from system engineering perspective. CO5: Demonstrate knowledge of basic system integration requirements.

II 18MTASD221 Introduction to

Aero Elasticity CO1 : Understanding of principles of vibration, elements of a vibrating system, classification of vibration , types of damping , free and forced vibration of undamped and damped single and two degree of freedom systems, principal coordinates, natural frequencies and mode shapes, normal modes, modal analysis etc. CO2 : Understanding of aeroelastic phenomenon and the multidisciplinary interactions involved, historical background, static aeroelastic phenomena like divergence, control effectiveness and reverasal , ability to model them, solution methods , extension to 3-D wings from 2-D airfoil models. CO3 : Understanding of dynamic aeroelastic phenomenon like flutter and ability to model and analyse them using simple two dimensional models and extension to 3-D flutter analysis.

II 18MTADE231 Introduction to Viscous Flow & Turbulence

CO1 : Apply concepts of boundary layer theory to fluid flow problems. CO2 :Apply statistical description of turbulent flows CO3 : Ability to analyze wall bounded flows, Free shear flows, Turbulent motion scales, velocity spectra. CO4 : Apply turbulence modeling theory

II 18MTAPT231 Materials and Processes for Propulsive Systems

CO1: Describe and suggest recommended materials for aero-engine components CO2: Explain desirable properties of different materials for engine components CO3: Recommend machining and sheet metal forming processes for engine components CO4: Recommend basic manufacturing process of tubular components of made of titanium alloy and composite honeycomb structures CO5: Suggest heat treatment processes of alloys used in engine components

II 18MTADE203 Basics of

Helicopters CO1: Understand the basic concepts associated with rotary wing aerodynamics. CO2 : Helicopter configurations based on various rotor classifications. CO3 : Aerodynamics & performance of helicopter in Hover, climb, descent, forward flight and autorotation. CO4 : Introduction to helicopter dynamics highlighting the interaction & coupling of aerodynamics and blade motions. CO5 : Basic helicopter controls and mechanism for achieving these controls. CO6 : Overview of static & dynamic stability of helicopter. CO7 : Sources of vibration of helicopter. Isolation and or reduction of vibrations.

II 18MTAPT203L Propulsion Lab CO1: To estimate and analyze heat transfer coefficient for forced convection over a flat plate and natural convection over an airfoil. CO2: To measure the pressure and velocity distribution in a convergent nozzle. CO3: To determine the growth rate of a free jet by finding the velocity profiles at different locations. CO4: To understand and plot starting characteristics of gas turbine engine in IIAEM. CO5: To understand and plot speed characteristics of gas turbine engine in IIAEM CO6: To determine the speed of premixed flame. CO7: To calculate pressure coefficient distribution over compressor blades

III 18MTAE301 Research Methodology

CO 1:Apply a range of quantitative and / or qualitative research techniques to business and management problems / issues. CO 2:Demonstrate knowledge and understanding of data analysis and interpretation in relation to the research process. CO 3:Conceptualise the research process. CO 4:Assess critically the following methods: literature study, case study, structured surveys, interviews, focus

groups, participatory approaches, narrative analysis, scenario methodology and basic statistical methods.

III 18MTAPT321 Airworthiness and Quality Control

CO1: Explain airworthiness requirements at aircraft level, system level, sub-system level and component level CO2: Will be able to support in the certification of aircraft and aircraft systems CO3: Will be able to support quality assurance procedures during manufacturing and testing of aircraft systems

III 18MTAPT322 Failure and Risk Analysis of Aero-Propulsion Systems

CO1. Explain the concept of failure and risk analysis with respect to engineering structures. CO2. Explain basic failure analysis methodology. CO3. Explain techniques for failure analysis CO4. Understand failures occurring during component testing and flight testing CO5. Carry out basic failure analysis of engine components

III 18MTAES303 IPR CO1:Understanding that when IPR would take such important place in growth of individuals & nation, it is needless to emphasis the need of information about Intellectual Property Right to be promoted among students in general & engineering in particular. CO2:Understand that IPR protection provides an incentive to inventors for further research work and investment in R & D, which leads to creation of new and better products, and in turn brings about, economic growth and social benefits

IV 18MTAEP304 Project work CO1: Will be able to carry out literature study of a propulsion system design project Co2: Will able to work in an industrial project that needs knowledge of aircraft propulsion systems

M.Tech in Aerospace Engineering – Aerodynamic Engineering Specialization


PEO 1: Graduates of the program will be able to lead teams or have a successful

professional career in industry/academia.

PEO 2: Graduates of the program will have the ability to pursue higher studies and

independently carry out research and development work to solve societal problems.

PEO 3: Graduates of the program will have the ability to design and implement solutions in

the area of aerodynamic engineering for rapidly changing technical requirements and lifelong

learning to adapt to innovation.


PSO 1: Graduates will possess skills in design, development and testing of aerodynamic

engineering.

PSO 2: Graduates will become professionally competent to take up real time projects

through aerospace industries.

PSO 3: Graduates will become globally competitive by pursuing research in the area of

avionics.


M.Tech in Aerodynamic Engineering 2018-20 batch

Semester

Course Code


I 18MTADE101

INTRODUCTION TO AEROSPACE VEHICLES

CO1 :To explain characteristics of airfoils, use of wind tunnel, basics if airplane stability, and Helicopters

CO2: To identify the materials used for aircraft structure and its structural layout

CO3: To explain working principles of different types of airbreathing propulsion systems and propulsion in helicopters

CO4: To explain major aircraft systems and aircraft navigational aids

CO5: To explain forces on a body in a central force field, rocket propulsion, and typical launch vehicle configurations

I 18MTMAE101

MATHEMATICS FOR AEROSPACE ENGINEERS

CO1 : Solve ordinary and partial differential equations using numerical techniques

CO2 : Apply principles of matrix algebra to linear transformations.

CO3 : Analyze the functions and signals using Fourier series and Fourier transforms

CO4 : Apply the concept of Calculus on Complex functions

I 18MTAS

D101 AEROSPACE STRUCTURES

CO1 : The students who learn the basics can handle the design of modern aircraft design

CO2 : The research career aspiring students have introduction to sufficient novel concepts from the course and they can embark on innovating work touching the frontiers of science.

CO3 : Sufficient learning will be acquired by the students o the computational aspects of Structural Mechanics

CO4 : Students gain confidence not to get scared and consequently refrain from using the modern aspects of structural science.

I 18MTADE102

AERODYNAMICS AND FLIGHT MECHANICS

CO1 : Modeling of bodies for aerodynamic analysis.

CO2 : Exposure to different airfoils, understating the influence of each of geometric parameter of the airfoil on aerodynamic forces & moments.

CO3 : Calculation of aircraft performance with specific reference to different speeds, range & endurance.

CO4 : Ability to do flight mechanics calculations.

I 18MTASD101L

AERO STRUCTURES LAB

CO1 : To measure the dimensions of various specimen by Vernier Caliper, Dial Gauge that finds applications in all the experiments.

CO2 : To enable the students to understand the various theorems and calculations based on Strength of Materials and Aircraft Structures approach.

CO3 : To study the fringe patterns of Stress and Strain using Photoelastic techniques.

CO4 : To understand the concepts of Vibrations and Elastic Stability.

I 18MTAPT102

AIRCRAFT PROPULSION

CO1 :Understand the basic principles of propulsion systems.

CO2 :Analyze the basic performance parameters of propulsion systems.

CO3 :Describe the design of propulsion systems

CO4 :Solve problems on design and performance of propulsion systems.

CO5 :Explain the working principles of different components of propulsion systems.

I 18MTAPT132

FAILURE AND RISK ANALYSIS OF AERO-PROPULSION

CO1 : Explain the concept of failure and risk analysis with respect to engineering structures.

CO2 : Explain basic failure analysis methodology.

CO3 : Explain techniques for failure analysis

CO4 : Understand failures occurring during component testing and flight testing

CO5 :. Carry out basic failure analysis of engine components

II 18MTADE201

COMPUTATIONAL FLUID DYNAMICS

CO1 : Derive governing equations for fluid flow. Learn various forms of governing equations and their significance.

CO2 :Classify partial differential equations and learn the properties.

CO3 :Learn different kinds of discretization methods for partial differential equations.

CO4 :Identify the conditions to be satisfied by the numerical scheme, consistency, stability and accuracy.

CO5 :Develop computer codes for Computational fluid dynamics.

II 18MTADE202

WIND TUNNEL THEORY AND TESTING

CO1 : Understanding fundamentals of design of different types of wind tunnels eg. Subsonic, transonic, supersonic and hypersonic, Blow down and suction types, open circuit and closed circuit; Aeronautical wind tunnel, water tunnel, environmental wind tunnels.

CO2 : Ability to plan & conduct wind tunnel experiments.

CO3 : Ability to collect and interpret wind tunnel data.

CO4 : Ability to apply flow visualization techniques using wind tunnel

II 18MTADE203

BASICS OF HELICOPTERS

CO1 : Understand the basic concepts associated with rotary wing aerodynamics.

CO2 : Helicopter configurations based on various rotor classifications.

CO3 : Aerodynamics & performance of helicopter in Hover, climb, descent, forward flight and autorotation.

CO4 : Introduction to helicopter dynamics highlighting the interaction & coupling of aerodynamics and blade motions.

CO5 : Basic helicopter controls and mechanism for achieving these controls.

CO6 : Overview of static & dynamic stability of helicopter.

CO7 : Sources of vibration of helicopter. Isolation and or reduction of vibrations.

II 18MTADE202L

WIND TUNNEL LAB

CO1 : Understanding fundamentals of design of different types of wind tunnels eg. Subsonic, transonic, supersonic and hypersonic, Blow down and suction types, open circuit and closed circuit; Aeronautical wind tunnel, water tunnel, environmental wind tunnels. - IA

CO2 : Ability to plan & conduct wind tunnel experiments

CO3 :Ability to collect and interpret wind tunnel data -

CO4: Ability to conduct flow visualization studies

II 18MTASD221

INTRODUCTION TO AEROELASTICITY

CO1 : Understanding of principles of vibration, elements of a vibrating system, classification of vibration , types of damping , free and forced vibration of undamped and damped single and two degree of freedom systems, principal coordinates,

natural frequencies and mode shapes, normal modes, modal analysis etc.

CO2 : Understanding of aeroelastic phenomenon and the multidisciplinary interactions involved, historical background, static aeroelastic phenomena like divergence, control effectiveness and reverasal , ability to model them, solution methods , extension to 3-D wings from 2-D airfoil models.

CO3 : Understanding of dynamic aeroelastic phenomenon like flutter and ability to model and analyse them using simple two dimensional models and extension to 3-D flutter analysis.

II 18MTADE222

FLIGHT TESTING - PERFORMANCE AND AERODYNAMICS

CO1 : Able to understand aircraft performance, flight testing, and aircraft performance evealuation at different flight conditions

CO2 : Apply flight testing techniques associated with stability requirements

CO3 :Apply flight testing procedures for helicopters

CO4 : Ability to undertake flight testing of aircraft components

CO5 : Apply flight data collection, reduction, analysis and reporting for aircraft.

II 18MTADE231

VISCOUS FLOWS AND TURBULENCE

CO1 : Apply concepts of boundary layer theory to fluid flow problems.

CO2 :Apply statistical description of turbulent flows

CO3 : Ability to analyze wall bounded flows, Free shear flows, Turbulent motion scales, velocity spectra.

CO4 : Apply turbulence modeling theory

II 18MTADE232

AIRPLANE STABILITY AND CONTROL

CO1 : To explain characteristics of airfoils, use of wind tunnel, basics if airplane stability, and Helicopters

CO2 : To identify the materials used for aircraft structure and its structural layout

CO3 : To explain working principles of different types of airbreathing propulsion systems and propulsion in helicopters.

CO4 : To explain major aircraft systems and aircraft navigational aids

CO5 : To explain forces on a body in a central force field, rocket propulsion, and typical launch vehicle configurations

III 18MTAE301

RESEARCH METHODOLOGY

CO1 : : Apply a range of quantitative and / or qualitative research techniques to business and management problems / issues

CO2 :Demonstrate knowledge and understanding of data analysis and interpretation in relation to the research process.

CO3 :Conceptualise the research process.

CO4 : Assess critically the following methods: literature study, case study, structured surveys, interviews, focus groups, participatory approaches, narrative analysis, scenario methodology and basic statistical methods.

III 18MTAES303

INTELLECTUAL PROPERTY RIGHTS

CO1 :Understanding that when IPR would take such important place in growth of individuals & nation, it is needless to emphasis the need of information about Intellectual Property Right to be promoted among students in general & engineering in particular.

CO2 :Understand that IPR protection provides an incentive to inventors for further research work and investment in R & D, which leads to creation of new and better products, and in turn brings about, economic growth and social benefits

III 18MTADE322

AEROSPACE DESIGN

CO1 : The students will be able to make layouts for payloads and systems and Estimate various loads acting on aircraft.

CO2 : Will be able to create preliminary structural design using aerodynamic load. and limit loads.

CO3 : Student will be able to estimate sizing and weight to calculate stresses, strains and displacements of critical structures, while subjected to allowable, limit and ultimate load.

CO4 : Knowledge on trends in Design, Manufacturing and testing in aerospace industry.

III 18MTADE321

HIGH SPEED AERODYNAMICS

CO1 : Calculate one dimensional flow properties, speed of sound and compressible flow relationships.

CO2 : Analysis of flow conditions involving normal shocks, oblique shock and expansion waves and their interactions.

CO3 : Apply various theories used to simplify the high speed flow analysis by linearization of governing equations.

CO4 : Apply slender body theory

CO5 : Analyse flow using method of characteristics and its use in design of high speed flow devices

CO6 : Analyse and apply experimental flow techniques for high speed flows

IV 18MTASP401

PROJECT WORK

CO1: Apply knowledge to identify, gather information to analyze and formulate the problem definition for project through detailed investigation.

CO2: Implement and demonstrate the defined project using appropriate tools

CO3 :Recommend sustainable solution/system for the betterment of the society, with scope for enhancement and continue life-long learning.

CO4: Defend the project through effective presentation with professional ethics as an individual or a member of a team

department of aerospace engineering b. tech in aerospace

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