First program concerns airframe vibratory loads encountered during flight tests of VZ-2 tilt-wing VTOL aircraft throughout operational range from hover to cruise flight; wing stall and tail buffeting in descents were primary sources of airframe vibrations; second program concerns initial results of structural loads survey conducted as wind tunnel test and deals with steady wing loads measured throughout simulated transition from hover to cruise.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural-loads surveys on two tilt-wing VTOL configurations


    Additional title:

    NASA -- Tech Note


    Contributors:
    Ward, J.F. (author)


    Publication date :

    1961


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    WING TILT SCHEDULING IN TANDEM-WING VTOL CONFIGURATIONS

    Grzedzinski, K. / Stephan, V. / Zolotas, A. | TIBKAT | 2021


    Tilt-wing VTOL aircraft

    McCormick, Jr., B.W. / Mallen, J. | Engineering Index Backfile | 1957


    Tilt-wing VTOL aircraft as commercial air transport

    Mazzitelli, F.R. | Engineering Index Backfile | 1957