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.


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    Titel :

    Structural dynamic and aeroelastic considerations for hypersonic vehicles


    Beteiligte:

    Kongress:

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


    Erscheinungsdatum :

    1991-06-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    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