A body of revolution, representing the equivalent area distribution of a low boom aircraft design cruising at 24,384 meters at a Mach number of 4, was tested to determine whether its theoretical sonic boom characteristics could be experimentally verified. Results indicate that the essential features of the ground signature are well predicted.


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    Titel :

    Wind Tunnel Test of Low Boom Equivalent Body at Mach 4


    Beteiligte:
    Howard, F. G. (Autor:in) / Morris, O. A. (Autor:in)

    Erscheinungsdatum :

    1974-09-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Sonic-Boom Wind-Tunnel Testing Techniques at High Mach Numbers

    ODELL A. MORRIS AND DAVID S. MILLER | AIAA | 1972



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