Aerodynamic Development of the Engine Nacelle Combination for the Boeing 767 Airplane
800731
04/01/1980
- Event
- Content
- 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.
- Pages
- 12
- Citation
- Neal, B., "Aerodynamic Development of the Engine Nacelle Combination for the Boeing 767 Airplane," SAE Technical Paper 800731, 1980, https://doi.org/10.4271/800731.