Feasibility of reducing one source of high intensity sound waves, namely exhaust of reciprocating air engine; silencer involves principle of high series inductance blocking pulsations, but allowing passage of steady flow and high shunt capacitance, bypassing or absorbing pulsations; exhaust silencer developed experimentally for Westland S.55 Whirlwind helicopter by Vokes Ltd. (see also Engineering v 179 n 4647 Feb 18 1955 p 217)


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    Title :

    Practical silencer design for piston engined aircraft


    Additional title:

    Am Helicopter


    Contributors:
    Vokes, G.H. (author)

    Published in:

    Publication date :

    1955


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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