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THE EVOLUTIONARY DEVELOPMENT AND CURRENT STATUS OF THE AUGMENTOR WING CONCEPT The Boeing Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Middlebrooks, J. E., author.
Conference Name:
National Aeronautic and Space Engineering and Manufacturing Meeting (1970-10-05 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1970
Summary:
A review is made of previously reported status of the augmentor wing concept, including test work of de Havilland Aircraft of Canada and the NASA Ames Research Center. More recent NASA data which formed the basis for proceeding with a flight research vehicle program on the Buffalo CV-7A are discussed. This background is used to show potential application to a turbofan-powered production airplane concept whose highly integrated propulsion and aerodynamics show promise for a very quiet STOL. Proposed future augmentor wing development programs are also briefly discussed
Notes:
Vendor supplied data
Publisher Number:
700812
Access Restriction:
Restricted for use by site license

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