The model nozzle configurations, acoustic test conditions, and detailed test results from the hot static and simulated flight acoustic tests at the General Electric Anechoc Chamber are described.


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    Title :

    Experimental Investigation of Shock-Cell Noise Reduction for Single-Stream Nozzles in Simulated Flight, Comprehensive Data Report. Volume 1: Test Nozzles and Acoustic Data


    Contributors:
    K. Yamamoto (author) / J. F. Brausch (author) / B. A. Janardan (author) / D. J. Hoerst (author) / A. O. Price (author)

    Publication date :

    1984


    Size :

    600 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English