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Computed Aeroelastic Motions Of Wings In Transonic FlowsReport describes computational simulations of aeroelastic motions of delta and swept wings in transonic flows. Study directed toward understanding aerodynamic behavior and enhancing maneuverability of fighter airplanes equipped with such wings. Also has implications for gas pumps and turbines, in which flows near tips of vanes and blades reach supersonic speeds.
Document ID
19950065456
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Guruswamy, Guru P.
(NASA Ames Research Center, Moffett Field, CA.)
Obayashi, Shigeru
(MCAT Institute)
Date Acquired
August 17, 2013
Publication Date
June 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 6
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-13191
Accession Number
95B10297
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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