Some of the specific areas associated with straight jet and turboprop engine installations are outlined where drag reduction and, thus, improved aircraft system performance is obtained. Specific areas constitute air intake sizing for general aviation aircraft, exhaust duct geometries and cooling system arrangements for propeller powered aircraft.
Installation drag considerations as related to turboprop and turbofan engines
1975-01-01
Conference paper
No indication
English
Low cost cargo aircraft -- Turboprop or turbofan ?
Engineering Index Backfile | 1960
|Comparison of advanced turboprop and turbofan airplanes
NTRS | 1983
|Comparison of Advanced Turboprop and Turbofan Airplanes
NTIS | 1983
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