With exhaust manifolds and efficient soundproofing treatment there is reasonable prospect of recommended standard being achieved at normal cruising speeds; exhaust noise may still be most important in frequency range from 75 to 600 cps, but at higher frequencies aerodynamic noise may predominate. (See also - (discussion) p 663-76; Aeroplane v 70 n 1821 Apr 19 1946 p 455-6; Mech World v 119 n 3097 May 10 1946 p 519-23)


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    Title :

    Silencing of aircraft


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Fleming, N. (author)

    Published in:

    Publication date :

    1946


    Size :

    25 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Silencing aircraft

    Davis, A.H. | Engineering Index Backfile | 1933


    Silencing aircraft

    Davis, Alfred H. | TIBKAT | 1933


    Silencing of aircraft

    Fleming, N. | Engineering Index Backfile | 1946


    AIRCRAFT SILENCING SYSTEM

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    Free access