In design of high speed aircraft, problem of relating structure loads to prescribed flight envelope leads often to necessity of airframes being considerably stronger than past experience suggests; one aspect of problem considered, namely, influence of elasticity upon aircraft derivatives from which tail loads are computed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aspect of deformation of swept wings in steady supersonic flight


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Hunn, B.A. (Autor:in) / Lance, G.N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1954


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Swept wings in supersonic flight

    Gates, S. B. | TIBKAT | 1954


    Swept wings in supersonic flight

    Gates, Sidney B. | SLUB | 1954



    Deformation analysis of tapered swept wings

    Hall, A.H. | Engineering Index Backfile | 1953


    Longitudinal stability of elastic swept wings at supersonic speed

    Frick, C.W. / Chubb, R.S. | Engineering Index Backfile | 1950