The aerodynamic development of the engine nacelle for the Boeing 767 airplane is described from configuration development model tests to FAA certification flight tests. Details of the inlet, nozzles and thrust reverser development in conjunction with the engine are discussed.
Aerodynamic Development of the Engine Nacelle Combination for the Boeing 767 Airplane
Sae Technical Papers
International Air Transportation Meeting ; 1980
1980-04-01
Aufsatz (Konferenz)
Englisch
1105-1135 Aerodynamic Nacelle Shape Optimization for NAL's Experimental Airplane
British Library Conference Proceedings | 2000
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