Structural dynamic and aeroelastic considerations applicable to hypersonic vehicles are discussed. Emphasis is given to aerospace plane configurations. The definition of aerothermoelasticity and the operational flight environment are reviewed, and structural dynamic and aeroelastic areas of concern are individually discussed, including vibration, landing and taxiing, propellant dynamics, acoustics, lifting surface flutter, panel flutter, control surface buzz, buffeting, gust response, and static aeroelasticity. Recent research results from all-moveable delta-wing aerolastic studies, engine inlet lip aeroelastic analysis, and studies of thermal effects on vibration frequencies, aerodynamic heating effects on flutter, and active control of aeroelastic response are reviewed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural dynamic and aeroelastic considerations for hypersonic vehicles



    Publication date :

    1991-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Structural Dynamic and Aeroelastic Considerations for Hypersonic Vehicles

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



    Structural dynamic and aeroelastic considerations for hypersonic vehicles

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