Sonic boom overpressures and signature duration may be predicted for the entire affected ground area for a wide variety of supersonic airplane configurations and spacecraft operating at altitudes up to 76 km in level flight or in moderate climbing or descending flight paths. The outlined procedure relies to a great extent on the use of charts to provide generation and propagation factors for use in relatively simple expressions for signature calculation. Computational requirements can be met by hand-held scientific calculators, or even by slide rules. A variety of correlations of predicted and measured sonic-boom data for airplanes and spacecraft serve to demonstrate the applicability of the simplified method.


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    Titel :

    Simplified sonic-boom prediction


    Beteiligte:
    Carlson, H. W. (Autor:in)

    Erscheinungsdatum :

    01.03.1978


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Simplified Sonic-Boom Prediction

    H. W. Carlson | NTIS | 1978


    Simplified sonic-boom prediction

    Carlson, Harry W. | TIBKAT | 1978


    Sonic Boom

    Maglieri, Domenic J. / Plotkin, Kenneth J. | NTRS | 1991



    Accurate Prediction of Sonic Boom Signals

    Pilon, Anthony | AIAA | 2006