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.


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    Title :

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


    Contributors:
    P. Garnero (author) / R. G. Lacau (author)

    Publication date :

    1992


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English