The specific geometrical, structural, and operational environment characteristics of hypersonic vehicles are discussed with particular reference to aerospace plane type configurations. A discussion of the structural dynamic and aeroelastic phenomena that must be addressed for this class of vehicles is presented. These phenomena are in the aeroservothermoelasticity technical area. Some illustrative examples of recent experimental and analytical work are given. Some examples of current research are pointed out.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural dynamic and aeroelastic considerations for hypersonic vehicles



    Conference:

    AIAA/ASME/ASCE/AHS/ASC 32d Structures, Structural Dynamics, and Materials Conference ; 1991 ; Baltimore, MD, United States


    Publication date :

    1991-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Structural dynamic and aeroelastic considerations for hypersonic vehicles

    Cazier, F. W., Jr. / Ricketts, Rodney H. / Doggett, Robert V., Jr. | NTRS | 1991


    Structural Dynamic and Aeroelastic Considerations for Hypersonic Vehicles

    F. W. Cazier / R. V. Doggett / R. H. Ricketts | NTIS | 1991



    Dynamic and aeroelastic considerations of hypersonic aircraft

    Rainey, A. G. / Martin, D. J. | NTRS | 1967


    Aeroelastic Simulation of Hypersonic Flight Vehicles

    Gupta, K. K. / Voelker, L. S. | AIAA | 2012