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Applications of oblique-wing technology - An overviewA summary of oblique-wing technology programs, including system studies and experimental activities, is presented. Oblique-wing civil transports were studied and compared with conventional configurations at design cruise Mach numbers of 0.95 and 1.2. Studies of military configurations employing oblique-wing technology considered aircraft concepts, remotely piloted vehicles, and a cruise missile. Experimental activities included wind-tunnel tests of high and low aspect ratio oblique wings; flight tests are planned using unmanned and manned vehicles. The research program suggests that oblique-wing technology offers improved performance over conventional concepts for aircraft operating in the transonic speed range.
Document ID
19760062451
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nelms, W. P., Jr.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 76-943
Accession Number
76A45417
Distribution Limits
Public
Copyright
Other

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