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An analytical study of effects on aeroelasticity on control effectivenessVarious uses of the Elastic Stability Derivative (ELASRAD) program are described. Topics include structural influence coefficient matrices of wings, arrow wing structural analysis, and graphic display of wing structures. The rigid and elastic stability derivatives were calculated for Transonic Aircraft Technology Project aircraft.
Document ID
19800015830
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mehrotra, S. C. (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-163197
Report Number: NASA-CR-163197
Accession Number
80N24322
Funding Number(s)
CONTRACT_GRANT: NSG-1046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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