Design program of combination suppressor-reverser having internal clamshell type reverser mounted between suppressor and engine; prototype configuration consists of basic pressure vessel mounting 21 individual nozzles to meet attenuation requirements of JT-3 engine; nozzle attenuation characteristics; design of 9-tube unit with very nearly same attenuation characteristics as 21-tube nozzle.


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    Titel :

    Design, development and operational experience of Boeing 707 thrust reverser/sound suppressor


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Barfoot, J.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1959 Thrust reversal



    Erscheinungsdatum :

    1959


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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