1 luchtvaart- en ruimtevaarttechniek | xx 2-10-2015 kick-off 2 nd year aerospace engineering

1Luchtvaart- en Ruimtevaarttechniek | xx

21-04-23

Kick-off 2nd year Aerospace Engineering

2Luchtvaart- en Ruimtevaarttechniek | 37| 37

Congratulations

You managed at least:


Contents today

• A small introduction• Global overview of the 2nd year• Per-module pitches by teachers – periods 1 + 2• Break + grab yourself some lunch• Per-module pitches by teachers – periods 3 + 4• Panel discussions / questions


Education Management Team

• Director of Education: Aldert Kamp• Head O&S: Madeleine Bos• Coordinator BSc 1: René Alderliesten• Coordinator BSc 2+3: René van Paassen• MSc Programme director: Leo Veldhuis• Student representative from the Society of Aerospace

Students

Academic Counsellors

Soc. Aerospace Students

Student Administration


Academic Counsellors

Open office hours: Mondays, Tuesdays and Thursdays from 12.30 till 14.00, high rise building, second floor.

Changes in availability are announced through Blackboard

Detailed contact information can be found on the AE Airport > Support > Academic Counsellors

Jill MoralesMerel Eggens

Susan de Rouw


BSc overview


2nd Year


From 1st to 2nd YearMaterials&structures

Calculus

Intro aerospace

Design

Mechanics

Physics

Linear Algebra

Python



Calculus

Intro aerospace

Design

Mechanics

Physics

Linear Algebra

Python


Summarizing

• The BSc 2nd year will bring a lot of exciting new topics• Figure out how things relate – what knowledge is required

+ adapt your study planning accordingly• Start thinking about your minor in the 3rd year; plan

ahead


21-04-23

Pitches first Semester:- Aerospace System Design- Aerodynamics (sub- and supersonic)- Differential Equations & Probability and Statistics- Structural and Vibrational Analysis & Design


AE2111 Module

AE2111-I AE2111-II

System Design

Aerospace Design and Systems Engineering Elements II

Nando Timmer Angelo Cervone

Durk Steenhuizen


AE2111-II ADSEE II

• Define what are the aircraft/spacecraft subsystems and

how do they function and interact

• Understand how to design some important subsystems,

putting them in a systems engineering context

General study goals


AE2111-II ADSEE II

After completing this course you will be able to perform a preliminary sizing of the aircraft wing and related sub-systems. In particular, the course will focus on:

•Wing functional requirements•Wing aerodynamic coefficients and characteristics•Airfoil shapes, taper ratio, aspect ratio, sweep and dihedral angles•Fuel systems, high lift devices, anti icing & de-icing systems

Specific study goals (aircraft)


AE2111-II ADSEE II

During this course you will learn some fundamental systems engineering principles and how to perform a preliminary sizing of two sub-systems: attitude determination/control and telecommunications. In particular:

•Space mission architecture, key spacecraft functions and subsystems•Functional analysis and requirements•Attitude fundamentals, sensors and actuators•Telecommunications technologies, link budget

Specific study goals (spacecraft)


AE2111-II ADSEE II

• Required knowledge: AE1222 – Aerospace Design and Systems Engineering

Elements I

• Educational method: One introduction lecture (1 hour) + 10 two-hour lectures

(5 on aircraft, 5 on spacecraft), weeks 1.1-1.2-1.3

• Assessment: Final exam, multiple choice + open questions (weight 4/6) Two homework group tutorials (weight 1/6 each): aircraft

in weeks 1.4-1.5, spacecraft in weeks 1.6-1.7 All assessment items are mandatory, and a grade of at

least 5.0 must be obtained in each

Practical matters


AE2130 “Aerodynamics”“Sub- and Supersonic”

• AE2130-I: “Aerodynamics 1” The basics of aerodynamics and incompressible flow theory

• AE2130-II: Low-speed wind tunnel practical

• AE2130-III: “Aerodynamics 2” High-speed aerodynamics


AE2130-I Aerodynamics 1The basics of aerodynamics

• Contents: • Basic concepts and the mathematical theory of

aerodynamics• Connection with low-speed aircraft theory (airfoils & wings)

• Learning goals: • How can we model, compute and predict flow behaviour?• How do airfoils/wings work?

• Teaching methods:• Lectures and exercises• Brush up on your maths!


AE2130-II Wind Tunnel PracticalLow speed wind tunnel experiment

• Contents: • Basic subsonic wind-tunnel testing• Practical and hands-on airfoil testing in the LTT windtunnel

• Learning goals: • How to measure aerodynamic properties in a windtunnel• What is the difference between 2D and 3D wing sections• How experiments compare to simulations

• Teaching methods:• 1 introductory lecture on basic concepts• 3-hour practical session of 8-10 student group in the LTT• Xfoil session


AE2130-III Aerodynamics 2High-speed aerodynamics

• Contents: • Shock & expansion waves• High speed wind tunnels & Nozzles• Transonic Aerodynamics

• Learning goals: • How can we model compressible flows• Understand essential phenomena• Prediction and computation of compressible

flows (airfoils, engine intakes, nozzles)

• Teaching methods:• Lectures, exercises and practical• Brush up on your thermo!


Module WI2180LR

Differential equations WI2180LR-IDifferential equations: Dynamics of structures such as aeroplanes

Important for aerodynamics;Turbulence;…

Probability & Statistics WI2180LR-IIProbability: Measure how likely it is that an event will happen.Statistics: Build models and interpret data.

Risk assessment and reliability engineering;Quality control;Forecast;….


Teaching and Assessment

Differential equations WI2180LR-ITeachingFrontal lectures: 6 hours, 6 weeks.AssessmentWritten exam: 8 short answer questions (NEW) + 3 open questions.

Probability & Statistics WI2180LR-IITeachingFrontal lectures: 2 hours, twice a week, 6 weeks.Tutorials: 2 hours, once a week, 6 weeks.Homework exercises.AssessmentThe final exam is multiple choice.Bonus: Non-mandatory graded tests along the course.


Required knowlegde

• CalculusDerivation and integration (also multivariate).

AE2135 Structural and Vibrational Analysis and Design

• AE2135 – I : Structural Analysis and Design (5 ECTS) Christos Kassapoglou

• AE2135 – II : Vibrations (3 ECTS) Sergio Turteltaub

This module is an introduction to analysis and design of aircraft structures under static or dynamic loads. It presents the basic principles which relate applied loads to displacements, stresses and strains. The characteristics of static and dynamic behaviour are discussed and methods to come up with designs that exhibit desirable characteristics are presented.

AE2135 – I Structural Analysis and DesignChristos Kassapoglou

• Application of material from previous courses:– Calculus (differentiation, integration, determination of max or min points,

functions of more than one variable…)– Differential equations (ODE’s, eigenvalue problems)– Statics (bending stresses, neutral axis, moment of inertia calculations,

shear stresses, …)– Materials (strength, yielding, von Mises stress)

• New material: Unsymmetric bending, buckling, torsion, shear, cutouts, tapered beams, energy methods (Castigliano’s theorems)

• Application to future courses: Simulation, Validation & Verification, graduate courses in structures

• In the end the student can: (a) Combine the above to analyse a given structure or (b) given applied loads, come up with a good (or optimum) design (geometry and material selection)

AE2135 – II VibrationsSergio Turteltaub

• For analysis and design purposes it is critical to model the dynamic response of a structure under free and forced loading conditions:– Vibrations and modelling of structures– Free and harmonically forced vibrations– Impulse loading, step loading, arbitrary

transient loading– Eigenfrequency, resonance, damping

• Required background: dynamics• Application to future courses:

– Simulation, Validation & Verification, graduate courses in structures

• In the end the student can:– Formulate and solve the equation of motion– Understand the influence of the main model

parameters on the structural response

• For analysis and design purposes it is critical to model the dynamic response of a structure under free and forced loading conditions:– Vibrations and modelling of structures– Free and harmonically forced vibrations– Impulse loading, step loading, arbitrary

transient loading– Eigenfrequency, resonance, damping

• Required background: dynamics• Application to future courses:

– Simulation, Validation & Verification, graduate courses in structures

• In the end the student can:– Formulate and solve the equation of motion– Understand the influence of the main model

parameters on the structural response


Break + grab yourself some lunch


21-04-23

Pitches Second Semester:- Test, Analysis & Simulation- Flight & Orbital Mechanics and Propulsion- Applied Numerical Analysis & Computational Modelling- Aerospace Signals, Systems & Control


AE2223 Module“Test, Analysis & Simulation”

• AE2223-I (project, period 3 & 4)Test analysis & Simulation•Data analysis and assessment of results•Scientific writing, communication of results

• AE2223-II (course, period 3)Experimental Research & Data Analysis•Design of experiments (numerical/physical)•Data analysis approaches


AE2223-ITest analysis & SimulationDr. Herman Damveld (C&O/C&S) & Dr. Ferry Schrijer (AWEP/AERO)

•Content and Learning goals: •Define research question based on literature investigation•Analysis of experimental and/or model results•Be able to draw conclusion in order to answer research question•Work in a research environment

•Teaching methods:•Project education (intro lecture, scientific writing sessions)•Reader & literature provided by tutor•Runs in periods 3 and 4

•Entrance requirements:•45 ECTs of the first year and AE1111-I and AE1222-I completed•Strongly recommended: programming course passed (AE1205)


AE2223-IIExperimental Research & Data AnalysisDr. Roger Groves (ASM/SIC) & Prof. Pieter N.A.M. Visser (SpE/AS)

•Content and Learning goals: •Design an experiment to test an hypothesis•Data analysis & error identification•Synthesis of results and draw conclusions about the hypothesis

•Teaching methods:•Lectures (period 3) and Assignments (e.g. 787 fatigue test, GPS)•Reader & slides•Written exam (period 3, resit period 4)•Intro. Aerosp. Eng, Calculus, Applied Num. Analysis, Prob. & Stat.


In order to participate in the AE2223-I project, it is mandatory to register through OSIRIS.

Go to OSIRIS > Register > Register for Course Module > Search a course module.

Registering for AE2223-I (Test, analysis and simulation) in OSIRIS is possible until November 27th, 2015.

Currently the registration is not yet open, please keep an eye out on blackboard for an announcement.


AE2230 Module

AE2230-I AE2230-II

Flight and Orbital

Mechanics

Propulsion and Power

Mark Voskuijl

Ron Noomen

Joris Melkert

Angelo Cervone


AE2230-I Flight and Orbital Mechanics

After completing this course you will be able to calculate accurate aircraft performance characteristics. For example:

•Minimum time needed to climb to cruise altitude•Runway distance needed for take-off and landing•Minimum turn radius•Fuel needed for a complete flight•Etc…

Study goals (1)



After completing this course you will be able to calculate the major characteristics of satellite trajectories. For example:

•Earth-repeat and Sun-synchronous orbits•Interplanetary transfers•Maneuvers•Timing of events•Etc…

Study goals (2)



• Required knowledge: AE1110 – Introduction to Aerospace Engineering

• Educational method: Two classical lectures per week

• Assessment: Final exam with open questions (calculations,

knowledge questions, analytical derivations)

Practical matters


AE2230-II Propulsion and Power

After completing this course, you will be able to understand the basic principles of thrust and power producing mechanisms for aerospace vehicles. In particular, the focus is on:

•Thermodynamics and cycle calculations•Gas turbine engines, turbo machinery, combustion•Electrical power systems (generators, solar cells, batteries, etc.)•Ideal rocket theory and space propulsion systems

Study goals


AE2230-II Propulsion and Power

• Required knowledge: AE1110 – Introduction to Aerospace Engineering AE1222 – Aerospace Design and Systems Engineering Elements I AE1240 - Physics

• Educational method: Two lectures per week (theory + demonstrations + exercises) Supporting videos on Blackboard

• Assessment: Final exam (mostly electronic), multiple choice + open questions Bonus assignments, spread through the whole course duration

Practical matters


Grading method AE2230 Module

AE2230-I Flight and Orbital Mechanics•You will have a regular exam•The final grade must be at least 5.0 to pass the course

AE2230-II Propulsion and Power•You will have a regular exam and several optional bonus assignments•The bonus assignments can give you a total maximum bonus of 1.0 point•Final grade = exam grade + bonus points•Bonus points are assigned only if the exam grade is 5.0 or higher•The final grade must be at least 5.0 to pass the course

AE2230 Module•The final grades for the individual courses will be rounded off to 1 decimal•The grade for the module is the average of the final grades for the individual courses, rounded off to half points

AE2220: Content

I: Applied Numerical Analysis→ Introduces the concepts and tools to numerically: Solve non-linear equations Interpolate, differentiate, and integrate Solve ordinary differential equations (ODEs) Solve optimisation problems

II: Computational Modelling→ Shows how to simulate physical systems described by PDEs using: Finite-difference methods Spectral and finite-element methods Time marching and iterative solution methods Verification/Error estimation techniques

AE2220: Format and Assessment

I: Applied Numerical Analysis Format: Lectures, python examples, homework problemsAssessment: 3 quizzes, or 1 resit exam

II: Computational ModellingFormat: Lectures, work sessions, mapleTA examplesAssessment: 3 quizzes + 3 work sessions,

or 3 quizzes, or 1 resit exam

AE2220: Prerequisites

A basic knowledge of: Python programming Calculus, linear algebra Differential equations


AE2235

• Aerospace Systems and Control Theory

• Instrumentation and Signals

AE2235-I : Aerospace Systems & Control Theory 45

https://www.youtube.com/watch?v=BhMSzC1crr0

Prof.dr.ir. Max Mulder, Dr.ir. Coen de Visser, Dr.ir. Rene van PaassenControl & Simulation

AE2235Aerospace Signals, Systems and Control


AE2235 Module in a Nutshell...

system

outputinput signal

control signal

Pilot controller

AE2235-I Instrumentation & Signals (Max Mulder)• Goal: Analyse signals in the time and frequency domain.

AE2235-II Aerospace Systems & Control Theory (Coen de Visser)

• Goal: Design control systems for aircraft, spacecraft, and drones. AE2235-I

AE2235-II


controller system

sensors

Pilot

output

measurements

AE2235 Module in a Nutshell...

( )H s( )y s( )c s( )u s

( )C s( )e s

Closed-loop control

mathematical conceptualizati

on

( )G s

( ) ( )( ) ( )

1 ( ) ( ) ( )

C s H sy s u s

C s H s G s


Dynamic System Analysis:

AE2235 Module Requirements

AE1130 Dynamics (equations of motion)

WI1403LR Linear Algebra (matrix manipulation)

AE2135-II Vibrations (second order differential equations)

WI2180LR-I Differential Equations (Laplace transform)

Signal Analysis:

WI2180LR-II Probability & Statistics (Stochastic signals)

Programming:

AE1205 Programming & Scientific Computing in Python


AE2235 Teaching & Assessment

AE2235-I Instrumentation & Signals (3 ECTS)• Lectures• Studio Classroom sessions with Python/Matlab • Written Exam

AE2235-II Aerospace Systems & Control Theory (4 ECTS)• Lectures• E-Lectures with Python/Matlab • Computer Exam with Python/Matlab


What will AE2235 do for you?

Signals and Control are Everywhere!


https://www.youtube.com/watch?v=XxFZ-VStApo

Prof.dr.ir Max Mulder, Dr.ir. Coen de Visser, Dr.ir. Rene van PaassenControl & Simulation

AE2235-I Aerospace Signals, Systems and Control

1 luchtvaart- en ruimtevaarttechniek | xx 2-10-2015 kick-off 2 nd year aerospace engineering

Documents

structural analysis

analysis simulationae2223

vibrational analysis

future courses

graduate courses

previous courses

structural response

ae2135 structural