Comparisons between computational results and other computational results or experimental measurements of supersonic flows around tactical missiles are given. The presented results concern: aerodynamics of air-breathing missiles; vortex flows around conventional missiles, and flows with lateral streams (a problem encountered with devices applying lateral thrust near the center of gravity). The codes used at AEROSPATIALE fall in two categories: linearized, supersonic potential codes; Euler codes (steady and unsteady).


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Calcul d'Ecoulements Supersoniques Autour de Missiles Tactiques (Calculation of Supersonic Flow around Tactical Missiles)


    Contributors:
    J. Lordon (author) / P. Guillen (author) / P. Mortel (author) / R. G. Lacau (author)

    Publication date :

    1986


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English