The stochastic model theory of TAM (1987, 1989) for broadband shock associated noise was extended to include the effects of forward flight. The theory was applied to the forward flight simulation experiments of Norum and Shearin (1984, 1986, and 1988). Good agreement is found between calculated and measured far-field noise spectra over the flight Mach number range of 0.0 to 0.4.


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    Title :

    Forward flight effects on broadband shock associated noise of supersonic jets


    Contributors:

    Publication date :

    1989-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :



    Broadband Shock Noise from Supersonic Jets

    T. D. Norum / J. M. Seiner | AIAA | 1982



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    Shock-associated noise in supersonic jets

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