Means of reducing or eliminating the sonic boom through aerodynamic design or aircraft operation are discussed. These include designing aircraft to minimize or eliminate certain features of the overpressure signature, operating aircraft at slightly supersonic speeds so that the sonic boom does not reach the ground, and seeking reductions through the high altitude-high speed flight conditions of hypersonic transports.


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    Titel :

    Sonic boom reduction through aircraft design and operation.


    Beteiligte:
    Seebass, A. R. (Autor:in) / George, A. R. (Autor:in)

    Kongress:

    Aerospace Sciences Meeting ; 1973 ; Washington, DC


    Erscheinungsdatum :

    1973-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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