The development of advanced CTOL aircraft engines with reduced exhaust emissions is discussed. Combustor noise information provided during the basic emissions program and used to advantage in securing reduced levels of combustion noise is included. Results are presented of internal pressure transducer measurements made during the scheduled emissions test program on ten configurations involving variations of three basic combustor designs.


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    Title :

    Noise addendum experimental clean combustor program, phase 1


    Contributors:
    Sofrin, T. G. (author) / Ross, D. A. (author)

    Publication date :

    1975-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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