To evaluate the oblique wing concept developed by Robert T. Jones and his associates at the NASA Ames Research Center, a flight test program has been initiated to assess the flying characteristics of a low speed manned oblique wing airplane. The principal objective of the program is to assess the aircraft's flying qualities at wing sweep angles from 0° to 60° and at indicated airspeeds up to 150 knots. At present the program is in the flight envelope expansion phase and is investigating flutter clearance as a function of wing sweep.


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    Titel :

    AD-1 OBLIQUE WING AIRCRAFT PROGRAM


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Sim, A.G. (Autor:in) / Felt, L.R. (Autor:in) / Monaghan, R.C. (Autor:in) / Smith, R.C. (Autor:in) / McMurtry, T.C. (Autor:in) / Andrews, W.H. (Autor:in)

    Kongress:

    Aerospace Congress and Exposition ; 1980



    Erscheinungsdatum :

    1980-09-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    AD-1 oblique wing aircraft program

    MCMURTRY, T. / SIM, A. / ANDREWS, W. | AIAA | 1981


    AD-1 oblique wing aircraft program

    Andrews, W. H. / Sim, A. G. / Monaghan, R. C. et al. | NTRS | 1980


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    Oblique-wing supersonic aircraft

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