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Low-Speed Characteristics of High-Performance Lift-Engine V/STOL Aircraft Ames Research Center, NASA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Barrack, Jerry P., author.
Conference Name:
National Aeronautic and Space Engineering and Manufacturing Meeting (1968-10-07 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1968
Summary:
Considerable research on large-scale high-performance, lift-engine, V/STOL configurations has been conducted at Ames Research Center. The exhaust gas reingestion characteristics, lift-engine inlet total-pressure recovery and distortion, and engine-airframe induced effects were measured in the 40 80 ft wind tunnel both in and out of ground effect over a wide range of transition flight conditions. The results of these investigations show that the lift-engine configurations studied may have severe operational constraints placed upon them during transition
Notes:
Vendor supplied data
Publisher Number:
680644
Access Restriction:
Restricted for use by site license

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