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Variable-Geometry Exhaust Nozzles and Their Effects on Airplane Performance AEG Engineering, General Electric Company
- Format:
- Conference/Event
- Author/Creator:
- Ammer, R. C., author.
- Conference Name:
- National Air Transportation Meeting (1968-04-29 : New York, New York, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1968
- Summary:
- The development of exhaust nozzles and their application in operational military aircraft are discussed. Prime consideration is given to installation factors such as engine bay and nozzle cooling, inlet-engine flow matching, and aerodynamic effects on external afterbody drag. Examples of various operational exhaust systems are given which show how the aircraft-exhaust nozzle characteristics are integrated to achieve maximum system compatibility and performance. Results from one flight test program are presented which show how an aircraft-exhaust nozzle system was integrated to achieve maximum installed performance
- Notes:
- Vendor supplied data
- Publisher Number:
- 680295
- Access Restriction:
- Restricted for use by site license
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