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Effect of leading-edge vortex flaps on aerodynamic performance of delta wingsThe effect of leading-edge vortex flaps on the aerodynamic characteristics of highly swept-back wings is analytically investigated, using the free vortex sheet method. The method, based on a three-dimensional inviscid flow model, is an advanced panel type employing quadratic doublet distributions to represent the wing surface, rolled-up vortex sheet and wake and is capable of computing forces, moments and surface pressures.
Document ID
19810060020
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Reddy, C. S.
(Old Dominion University Norfolk, VA, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Publication Information
Publication: Journal of Aircraft
Volume: 18
Subject Category
Aerodynamics
Accession Number
81A44424
Funding Number(s)
CONTRACT_GRANT: NSG-1561
Distribution Limits
Public
Copyright
Other

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