Discussion of sensitivity of SST design and operation to sonic-boom considerations shows necessity for study of problems early in development program; methods of predicting pressure signatures are outlined and examples of correlation of estimates with wind-tunnel and flight measurements are shown; estimates of sonic-boom characteristics for SST show that in critical transonic acceleration portion of flight, overpressures somewhat lower than estimated by use of far-field assumptions may be expected.


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    Titel :

    Prediction of airplane sonic-boom pressure fields


    Weitere Titelangaben:

    NASA SP


    Beteiligte:
    Carlson, H.W. (Autor:in) / McLean, F.E. (Autor:in) / Middleton, W.D. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Prediction of Airplane Sonic-Boom Pressure Fields

    Carlson, Harry W. / McLean, F. Edward / Middleton, Wilbur D. | NTRS | 1965


    Prediction of airplane sonic-boom pressure fields

    Carlson, H. W. / Mc Lean, F. E. / Middleton, W. D. | NTRS | 1965




    Sonic boom loudness study and airplane configuration development

    Brown, Jessica G. / Haglund, George T. | NTRS | 1988