Aircraft has to fit following flight regimes; orbital, hypersonic, supersonic transonic, and subsonic + landing; selection of right compromises between often contradictory conditions; problem of longitudinal stability; subsonic and hypersonic lift-drag ratio and aerodynamic heating are examined; it is shown that hypersonic lift drag ratio has to be determined by restraints which aerodynamic heating problem imposes on design.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design of hypersonic aircraft


    Weitere Titelangaben:

    Aero/Space Eng


    Beteiligte:
    Multhopp, H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Hypersonic Aircraft Design

    H. Alkamhawi / T. Greiner / G. Fuerst et al. | NTIS | 1990


    Hypersonic aircraft design

    Alkamhawi, Hani / Greiner, Tom / Fuerst, Gerry et al. | NTRS | 1990


    Advanced hypersonic aircraft design

    Utzinger, Rob / Blank, Hans-Joachim / Cox, Craig et al. | NTRS | 1992


    Advanced Hypersonic Aircraft Design

    R. Utzinger / H. Blank / C. Cox et al. | NTIS | 1992


    Design of hypersonic aircraft

    Swithenbank, J. | Engineering Index Backfile | 1964