Currently in aeronautics the aims and objectives of wind tunnels experiment are diverse. It could be purely for optimising the aerodynamic design at the high speeds (transonic for the transport aircraft) by conceiving efficient wing sections, coupling the structure and aerodynamics (optimised volume, lighter structure, aeroelastic behaviour), developing innovative deployable surfaces to achieve high lift at low speed, controlling the plane’s behaviour (performance, manoeuvrability and flight envelope) up to maximum lift coefficient and beyond stall. In the field of terrestrial vehicles, the objectives are to decrease the drag in order to reduce the fuel consumption, to guarantee the stability of the vehicle (response to cross wind) and to increase interior comfort by reducing aerodynamic noise.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Computer-Aided Wind Tunnel Test and Analysis


    Weitere Titelangaben:

    Springer Tracts in Mechanical Engineering


    Beteiligte:
    Chanetz, Bruno (Autor:in) / Délery, Jean (Autor:in) / Gilliéron, Patrick (Autor:in) / Gnemmi, Patrick (Autor:in) / Gowree, Erwin R. (Autor:in) / Perrier, Philippe (Autor:in)


    Erscheinungsdatum :

    03.01.2020


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Modelling Tunnel Diodes for Computer Aided Design

    Abuelma'atti, M. T. / Ali, A. R. | British Library Online Contents | 1993



    SAMPSON smart inlet design overview and wind tunnel test: II. Wind tunnel test

    Pitt, Dale M. / Dunne, James P. / White, Edward V. | SPIE | 2002