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Computation Of Flow About A Pitching Wing/FuselageReport presents computational study of unsteady transonic flow about airplanelike body as body pitches upward in increasing angle of attack.
Document ID
19960022429
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Obayashi, S. (NASA Ames Research Center, Moffett Field, CA.)
Guruswamy, G. P. (NASA Ames Research Center, Moffett Field, CA.)
Tu, E. L. (NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 17, 2013
Publication Date
May 1, 1996
Publication Information
Publication: NASA Tech Briefs
Volume: 20
Issue: 5
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-13172
Report Number: ARC-13172
ISSN: 0145-319X
Accession Number
96B10244
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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