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A parametric study of planform and aeroelastic effects on aerodynamic center, alpha- and q- stability derivatives. Appendix D: Procedures used to determine the mass distribution for idealized low aspect ratio two spar fighter wingsThe procedures used to establish the mass matrices characteristics for the fighter type wings studied are given. A description of the procedure used to find the mass associated with a specific aerodynamic panel is presented and some examples of the application of the procedure are included.
Document ID
19730013173
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roskam, J. (Kansas Univ. Lawrence, KS, United States)
Hamler, F. R. (Kansas Univ. Lawrence, KS, United States)
Reynolds, D. (Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-112232
CRINC-FRL-72-014-APP-D
Accession Number
73N21900
Funding Number(s)
CONTRACT_GRANT: NGR-17-002-071
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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