Design philosophy applied by Lockheed-California Co in selecting double-delta wing planform as optimum for supersonic transports with regard to economics, community acceptability, and safety; passenger capacity considerations lead to choice of fuselage size; wing affects economy to large degree through lift-to-drag ratio, speed, and weight, and influences sonic boom and airport noise; it determines flying qualities and degree of simplicity which can be achieved; operational characteristics and takeoff, approach and landings considerations; speed stability and factors to take into account.


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    Titel :

    Performance and flying qualities of double-delta supersonic transport


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Heppe, R.R. (Autor:in) / Magruder, W.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Supersonic



    Erscheinungsdatum :

    1964


    Format / Umfang :

    20 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Performance and Flying Qualities of the Double-Delta Supersonic Transport

    Heppe, R. R. / Magruder, W. M. | SAE Technical Papers | 1964


    Impact of Structural Vibration on Flying Qualities of a Supersonic Transport

    D. L. Raney / E. B. Jackson / C. S. Buttrill et al. | NTIS | 2001



    Supersonic Flying Qualities Experience Using the SR-71

    Cox, T. / Jackson, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1997


    Supersonic flying qualities experience using the SR-71

    Cox, Timothy / Jackson, Dante | AIAA | 1997