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.
Engine installation problems in XP-84 airplane
Soc Automotive Engrs -- Trans
1948
Article (Journal)
English
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