Set of curves presented from which stagnation-point equilibrium wall temperature during rocket-powered ascent, steady-state hypersonic flight, and re-entry, can be derived; most ballistic missile trajectories fall within range covered by these curves.


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    Titel :

    Figuring heating of blunt shapes in hypersonic flight


    Weitere Titelangaben:

    Space/Aeronautics


    Beteiligte:
    Wing, L.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Induced pressures and shock shapes on blunt cones in hypersonic flow

    Wagner, Richard D. / Watson, Ralph | TIBKAT | 1964


    Hypersonic Interference Heating Induced by a Blunt Fin

    Schuricht, P. H. / Roberts, G. T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1998


    Hypersonic interference heating induced by a blunt fin

    Schuricht, P. / Roberts, G. | AIAA | 1998


    Shock Shapes of Blunt Bodies in Hypersonic Helium, Air, and CO, Flows

    CHARLES G. MILLER AND JOHN A. MOORE | AIAA | 1974