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A vortex-lattice method for calculating longitudinal dynamic stability derivatives of oscillating delta wingsPreviously cited in issue 21, p. 3626, Accession no. A81-44570
Document ID
19840034639
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Levin, D. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Publication Information
Publication: AIAA Journal
Volume: 22
ISSN: 0001-1452
Subject Category
Aircraft Stability And Control
Report/Patent Number
ISSN: 0001-1452
Accession Number
84A17426
Distribution Limits
Public
Copyright
Other

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