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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1959 Thrust reversal



    Publication date :

    1959


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Boeing jet thrust reverser

    Evans, S.H. | Engineering Index Backfile | 1954



    Development of the Boeing 767 thrust reverser

    Jackson, J. | Tema Archive | 1987


    Boeing 777 thrust reverser actuation system

    O’Brien, Mike | Emerald Group Publishing | 1998