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Flutter: A finite element program for aerodynamic instability analysis of general shells of revolution with thermal prestressDocumentation for the computer program FLUTTER is presented. The theory of aerodynamic instability with thermal prestress is discussed. Theoretical aspects of the finite element matrices required in the aerodynamic instability analysis are also discussed. General organization of the computer program is explained, and instructions are then presented for the execution of the program.
Document ID
19830011485
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fallon, D. J. (Old Dominion Univ. Norfolk, VA, United States)
Thornton, E. A. (Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:170013
NASA-CR-170013
Report Number: NAS 1.26:170013
Report Number: NASA-CR-170013
Accession Number
83N19756
Funding Number(s)
CONTRACT_GRANT: NSG-1167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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