As flight envelope has expanded, increasing number of possible applications of variable geometry devices has developed; aerodynamic factors have been shown to present some difficulty in using variable sweep wings in strictly subsonic areas of slow flight, maneuvering and best cruise; they, and other variable geometry devices, offer considerable promise in maintaining good subsonic characteristics while minimizing supersonic drag (either at low lift or near maximum L/D) or effecting desired stability margins.


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    Titel :

    Aerodynamic design considerations of variable geometry aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Landgraf, S.K. (Autor:in) / Herring, R.N. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Design



    Erscheinungsdatum :

    1967


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic Design Considerations of Variable Geometry Aircraft

    Herring, R. N. / Landgraf, S. K. | SAE Technical Papers | 1967


    Maintainability Considerations in Variable Geometry Aircraft

    Onewein, L. J. | SAE Technical Papers | 1967


    Maintainability considerations in variable geometry aircraft

    Onewein, L.J. | Engineering Index Backfile | 1967


    Aerodynamic design considerations for aircraft radomes

    GIRAGOSIAN, PAKRAD / LOOS, SCOTT | AIAA | 1990


    Aircraft aerodynamic design : geometry and optimization

    Sóbester, András / Forrester, Alexander I. J. | TIBKAT | 2015