Modes of failure found to be significant are considered which can be either aerodynamic, dynamic, structural, or combination of all 3; example of aero-thermal-elastic effects changing stability derivatives; when wing is exposed to loads and temperatures of selected flight profile, thermal deflections can be calculated using given temperature distribution; throughout mission profile, stability derivatives are changing and, thus, stability boundaries.


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    Title :

    Modes of failure of hypersonic re-entry glide vehicle


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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