The Tactical Missile Division has been using ramjets on its missiles for more than thirty years. The adaptation of this type of propulsion to very high speed aircraft and airbreathing launchers is investigated. We must study vehicles designed for higher and higher speeds, and we need to optimize more rapidly, and at a lower cost, our airbreathing missile configurations. We completed our supersonic air intake design methodology by using CFD for our work in external and internal aerodynamics. These CFD tools involving Euler and Navier-Stokes codes and mesh generators are complementary to wind tunnel tests.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Etudes Aerodynamiques de Prises d'Air Supersoniques (Aerodynamic Studies of Supersonic Air Intakes)


    Beteiligte:
    P. Garnero (Autor:in) / R. G. Lacau (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch