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.


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    Titel :

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


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Wykes, J.H. (Autor:in) / Lawrence, R.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :