wing cfd analysis (2)

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    CFD analysis of subsonic aircraft wing

    part.

    Hardeep Zinta,

    Supervisor:-Assistant Prof. Geremes.Y.N

    (XAI) National Aerospace University

    Ministry of education and sciences of Ukraine.

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    Introduction Analysis Result Conclusion

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    IntroductionComputational fluid dynamics, usually abbreviated as CFD, is a

    branch offluid mechanicsthat usesnumerical methodsand

    algorithmsto solve and analyze problems that involvefluid flows.

    Computers are used to perform the calculations required to

    simulate the interaction of liquids and gases with surfaces defined

    byboundary conditions. With high-speedsupercomputers, better

    solutions can be achieved. Ongoing research yields software that

    improves the accuracy and speed of complex simulation scenarios

    such astransonicorturbulentflows. Initial experimental validation

    of such software is performed using awind tunnelwith the final

    validation coming in full-scale testing, e.g.flight tests.

    https://en.wikipedia.org/wiki/Fluid_mechanicshttps://en.wikipedia.org/wiki/Fluid_mechanicshttps://en.wikipedia.org/wiki/Fluid_mechanicshttps://en.wikipedia.org/wiki/Numerical_methodshttps://en.wikipedia.org/wiki/Numerical_methodshttps://en.wikipedia.org/wiki/Numerical_methodshttps://en.wikipedia.org/wiki/Algorithmshttps://en.wikipedia.org/wiki/Algorithmshttps://en.wikipedia.org/wiki/Fluid_dynamicshttps://en.wikipedia.org/wiki/Fluid_dynamicshttps://en.wikipedia.org/wiki/Fluid_dynamicshttps://en.wikipedia.org/wiki/Boundary_conditionshttps://en.wikipedia.org/wiki/Boundary_conditionshttps://en.wikipedia.org/wiki/Boundary_conditionshttps://en.wikipedia.org/wiki/Supercomputerhttps://en.wikipedia.org/wiki/Supercomputerhttps://en.wikipedia.org/wiki/Supercomputerhttps://en.wikipedia.org/wiki/Transonichttps://en.wikipedia.org/wiki/Transonichttps://en.wikipedia.org/wiki/Transonichttps://en.wikipedia.org/wiki/Turbulencehttps://en.wikipedia.org/wiki/Turbulencehttps://en.wikipedia.org/wiki/Turbulencehttps://en.wikipedia.org/wiki/Wind_tunnelhttps://en.wikipedia.org/wiki/Wind_tunnelhttps://en.wikipedia.org/wiki/Wind_tunnelhttps://en.wikipedia.org/wiki/Flight_testhttps://en.wikipedia.org/wiki/Flight_testhttps://en.wikipedia.org/wiki/Flight_testhttps://en.wikipedia.org/wiki/Flight_testhttps://en.wikipedia.org/wiki/Wind_tunnelhttps://en.wikipedia.org/wiki/Turbulencehttps://en.wikipedia.org/wiki/Transonichttps://en.wikipedia.org/wiki/Supercomputerhttps://en.wikipedia.org/wiki/Boundary_conditionshttps://en.wikipedia.org/wiki/Fluid_dynamicshttps://en.wikipedia.org/wiki/Algorithmshttps://en.wikipedia.org/wiki/Numerical_methodshttps://en.wikipedia.org/wiki/Fluid_mechanics
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    Some examples are:-

    1. aerodynamics of aircraft and vehicles: lift and drag

    numerical simulation of an aircraft in German aerospace center(DLR).

    2. Hydrodynamics of ships.

    Cfd model of ship.

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    3. power plant

    A CFD model simulating the flow and pressure in a reactor coolant pump at the Loviisa nuclear

    power plant. The effect of modifications was simulated using the model prior to actual work being

    carried out.

    4. Biomedical engineering

    More recently, Computational Fluid Dynamics (CFD) has emerged as a promising tool, which,

    alongside experimentation, can yield insights of unprecedented detail into the hemodynamics of

    prosthetic heart valves

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    Analysis:-

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    Theory-

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    Momentum equaon 2

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    ModelHere we are importing geometry from CAD

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    Enclosure

    Here we are taking 400mm enclosure uniformly surrounding the model.

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    MeshingIn this component we are doing mesh of the model in 100 relevance.

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    Set up

    Doman(fluid, solid)boundary condition in fluid Doman(inlet,outlet,walls)we are

    testing wing in subsonic wind tunnel, so we are putting air speed in inlet is

    equal to 0.75 Mach and static pressure in outlet is equal to zero.

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    Solve-we are running salutation in current data and here we are obtaining following

    graphs.

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    Result-In this section we obtain velocity vector, velocity streamline,counter pressure and counter velocity.

    velocity vector

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    velocity streamline.

    pressure contour.

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    velocity contour.

    Conclusion.Here we are getting very high pressure in engine nacelle and front

    edges of the wing and it can affect wing structure and wing skin also.so

    we need here batter design salutation who will support wing shape

    aerodynamically.

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    References.1.

    CFD Notes, Dr. PK Dyson.

    2.ANSYS CFX Tutorials.

    3.An Introduction to Computational Fluid

    Dynamics,H.K.Versteeg and Malalasekera.

    4.Applied Computational Fluid Dynamics Techniques.

    5.Wikipedia

    6. http://www.cfd-online.com