Special muffler having 600-ft cross section for reduction of intense noise from burning of jet engine in test section of supersonic wind tunnel at Lewis Flight Propulsion Laboratory in Cleveland.


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    Title :

    Noise control for NACA supersonic wind tunnel


    Additional title:

    Acoustical Soc America -- J


    Contributors:
    Beranek, L.L. (author) / Labate, S. (author) / Ingard, U. (author)


    Publication date :

    1955


    Size :

    14 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Acoustical treatment for NACA 8- by 6-foot supersonic propulsion wind tunnel

    Beranek, L.L. / Labate, S. / Ingard, U. et al. | Engineering Index Backfile | 1955


    Acoustical Treatment for the NACA 8- by 6-foot Supersonic Propulsion Wind Tunnel

    Beranek, Leo L / Labate, Samuel / Ingard, Uno | NTRS | 1955


    Acoustical treatment for the NACA 8-by-6-foot supersonic propulsion wind tunnel

    Beranek, Leo L. / Labate, Samuel / Ingard, Uno | TIBKAT | 1955


    NACA transonic wind-tunnel test sections

    Wright, Ray H. / Ward, Vernon G. | TIBKAT | 1955


    NACA transonic wind tunnel test sections

    Wright, Ray H. ;Ward, Vernon G. | SLUB | 1956