Calculations of responses to continuous turbulence of B-47A airplane were compared with flight test results; calculations, based on 5° of freedom, lifting-surface aerodynamics for non-steady subsonic flow, and one-dimensional turbulence agree favorably with flight test results; method of calculation should give results of corresponding accuracy when applied to similar configurations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Calculated responses of large sweptwing airplane to continuous turbulence with flight-test comparisons


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Bennett, F.V. (Autor:in) / Pratt, K.G. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :