A 1/3 scale model static test program was conducted to measure the noise levels and reverse thrust performance characteristics of wing-mounted thrust reverser that could be used on an advanced augmentor wing airplane. The configuration tested represents only the most fundamental designs where installation and packaging restraints are not considered. The thrust reverser performance is presented in terms of horizontal, vertical, and resultant effectiveness ratios and the reverser noise is compared on the basis of peak perceived noise level (PNL) and one-third octave band data (OASPL). From an analysis of the model force and acoustic data, an assessment is made on the stopping distance versus noise for a 90,900 kg (200,000 lb) airplane using this type of thrust reverser. (Author)


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    Title :

    Static Performance and Noise Tests on a Thrust Reverser for an Augmentor Wing Aircraft


    Contributors:
    D. L. Harkonen (author) / C. C. Marrs (author) / J. V. Okeefe (author)

    Publication date :

    1974


    Size :

    86 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Static performance and noise tests on a thrust reverser for an augmentor wing aircraft

    Harkonen, D. L. / Marrs, C. C. / Okeefe, J. V. | NTRS | 1974




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