First part deals with low speed aerodynamics of aircraft shapes suggested by D.Kuechemann as suitable for achieving required range at supersonic speeds, viz, wingbody arrangements with sweepback angles of 55 or 60° and streamwise thickness chord ratio of about 5%, suitable for low supersonic speed, and slender near triangular wings with sharp leading edges suitable for 2 Mach or more; second part is concerned with work aimed at clarifying requirements for handling qualities of future aircraft.


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    Titel :

    Some low speed problems of high speed aircraft


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Spence, A. (Autor:in) / Lean, D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    15 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Some low-speed problems of high-speed aircraft

    Spence, A. / Lean, D. | Engineering Index Backfile | 1961


    Some problems in design of high-speed aircraft

    Leonard, L.H. | Engineering Index Backfile | 1938


    Some problems in design of high-speed aircraft

    Leonard, L.H. | Engineering Index Backfile | 1938


    Some Elevated Temperature Structural Problems of High-Speed Aircraft

    Heldenfels, Richard R. | SAE Technical Papers | 1956


    Flutter problems of high-speed aircraft

    Broadbent, E. G. / Aeronautical Research Council | TIBKAT | 1955