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Lifting-line theory of oblique wingsThe study extends Prandtl's lifting-line theory to planar wings involving swept and curved centerlines. Attention is focused on distinct features of such a theory, with special emphasis on an oblique wing in a steady incompressible potential flow. The analysis presented is compared with exact solutions derived from an inverse method and with results from a panel method.
Document ID
19790029975
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cheng, H. K.
(Southern California, University Los Angeles, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1978
Publication Information
Publication: AIAA Journal
Volume: 16
Subject Category
Aerodynamics
Accession Number
79A13988
Funding Number(s)
CONTRACT_GRANT: N00014-75-C-0520
CONTRACT_GRANT: NCA2-OR730-601
Distribution Limits
Public
Copyright
Other

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