Results of investigations of flow in wake of hypersonic vehicles; nonsimilar solutions of equations governing "far wake" are obtained, and numerical results for flow field in wake of ballistic range and wind-tunnel models and of flight-size vehicle; ballistic range experiments with conical models of 10°, 15°, and 27 1/2 ° semivertex angles are described; model velocity ranges between 4000 and 17,000 fps with range pressures varying from 15 to 330 mm of Hg in air; analysis is used to compute and correlate transition parameters; predictions of location of transition in wake of 12° semivertex angle cone at 22,000 fps are made for altitude range from 200,000 to 100,000 ft.


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    Titel :

    Hypersonic laminar wakes and transition studies


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Pallone, A. (Autor:in) / Erdos, J. (Autor:in) / Eckerman, J. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 5


    Erscheinungsdatum :

    1964


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Hypersonic laminar wakes and transition studies

    ECKERMAN, J. / ERDOS, J. / PALLONE, A. | AIAA | 1964


    HYPERSONIC LAMINAR WAKES AND TRANSITION STUDIES

    PALLONE, A. / ERDOS, J. / ECKERMAN, J. | AIAA | 1963


    Computational probing of hypersonic laminar wakes

    REKLIS, R. / CONTI, R. | AIAA | 1984