Paper shows that most efficient use of weight in vehicle design will only be achieved through examination of aerothermoelastic problem areas early in design cycle; emphasis is on effects associated with longitudinal stability and control of possible supersonic transport canard-delta configuration; flexible-to-rigid-ratio data obtained from modal techniques are presented for most major aerodynamic parameters at two loading conditions; direct influence coefficient approach provided additional insight into component mass and aerodynamic influences.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerothermoelasticity -- Its impact on stability and control of winged aerospace vehicles


    Additional title:

    J Aircraft


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :