During process of entering planetary atmospheres, space vehicles may encounter largest flight dynamic pressures at very high Mach numbers; most severe aeroelastic phenomena may therefore occur at hypersonic speeds; 2 approximate techniques described hold promise of supplying information of dynamic airload prediction for 2- and 3-dimensional pointed bodies of general shape; illustrations including comparisons and application to chordwise divergence.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Dynamic airloads and aeroelastic problems at entry Mach numbers


    Additional title:

    J Aerospace Sciences


    Contributors:
    Zaratarian, G. (author) / Hsu, P.T. (author) / Ashley, H. (author)

    Published in:

    Publication date :

    1961


    Size :

    14 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    DEVELOPMENT OF AN AEROELASTIC METHOD FOR PREDICTING ROTOR AIRLOADS AND STRUCTURAL LOADS

    Su, J.C. / Zhang, F. / International Council of the Aeronautical Sciences; Optimage Ltd | British Library Conference Proceedings | 2010


    COMPARISONS OF FULLY COUPLED AEROELASTIC FUSELAGE SIMULATIONS TO UH-60A AIRLOADS PROGRAM DATA

    Reveles, N. / Pierce, T. / Blades, E. et al. | British Library Conference Proceedings | 2020


    Dynamic and aeroelastic problems of lifting re-entry bodies

    Hedgepeth, J. / Widmayer, Jr., E. | Engineering Index Backfile | 1963