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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    NASA -- Tech Report


    Contributors:
    Bennett, F.V. (author) / Pratt, K.G. (author)


    Publication date :

    1960


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :