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An attached flow design of a noninterfering leading edge extension to a thick delta wingThe analytical procedure presented for leading edge extension (LEE) determination, in keeping with such design criteria as noninterference at the wing design point, is applied to thick delta wings. The LEE device thus defined is to be mounted on a wing along a dividing stream surface that is associated with an attached flow design lift coefficient greater than zero. The delta wing in question is of twisted and cambered type. It is demonstrated that span reductions for the candidate LEEs has the most detrimental effect on overall aerodynamic efficiency, irrespective of area or shape.
Document ID
19850037538
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ghaffari, F.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Lamar, J. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-0350
Accession Number
85A19689
Distribution Limits
Public
Copyright
Other

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