Simulated flight experiments to Mach 0.4 on underexpanded jets show that flight has only minor effects on both the shock structure and shock associated noise. Although screech modes that do not exist statically become dominant at the higher flight speeds, the screech amplitudes and directivity as well as the broadband shock noise amplitudes remain relatively constant as the forward speed is increased. The change in wavelength due to flight on both shock noise components are predicted well from existing theories of shock noise.


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    Title :

    Shock noise from supersonic jets in simulated flight to Mach 0.4


    Contributors:

    Publication date :

    1986-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :