Difficulties encountered by both General Electric and Republic Aviation with TG-180 in P-84 Thunderjet; provision for quick engine replacement; reduction of losses in long inlet duct; development of joint for tail pipe and engine; choice of thermal protection for fuselage: provision for adjusting tail pipe area; design of fuel system; suggestions for improving design from installation standpoint.


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    Title :

    Engine installation problems in XP-84 airplane


    Additional title:

    Soc Automotive Engrs -- Trans


    Contributors:


    Publication date :

    1948


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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