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 Am Helicopter v 37 n 3 Feb 1955 p 6-7, 12-3)


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    Titel :

    Practical silencer design for piston engined aircraft


    Weitere Titelangaben:

    Engineering


    Beteiligte:
    Vokes, G.H. (Autor:in)

    Erschienen in:

    Engineering ; 179 , n 4647


    Erscheinungsdatum :

    1955


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Practical silencer design for piston engined aircraft

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