NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wingsCharts and approximate formulas are presented for the estimation of aeroelastic effects on the spanwise lift distribution, lift-curve slope, aerodynamic center, and damping in roll of swept and unswept wings at subsonic and supersonic speeds. Some design considerations brought out by the results of this report are discussed.
Document ID
19930092169
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Diederich, Franklin W
Foss, Kenneth A
Date Acquired
September 6, 2013
Publication Date
January 1, 1953
Report/Patent Number
NACA-TR-1140
Report Number: NACA-TR-1140
Accession Number
93R21459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitleNACA-TN-2608Superseded By
No Preview Available