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Low-speed aerodynamic characteristics of a highly swept arrow wing configuration with several deflected leading edge conceptsThe effectiveness of leading edge concepts for minimizing or controlling leading edge flow separation was studied. Emphasis was placed on low speed performance, stability, and control characteristics of configurations with highly swept wings. Simple deflection of the leading edge, a variable camber leading edge system, and a leading edge vortex flow system were among the concepts studied. The data are presented without analysis.
Document ID
19800024839
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gentry, G. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Coe, P. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-80180
Report Number: NASA-TM-80180
Accession Number
80N33347
Funding Number(s)
PROJECT: RTOP 533-01-43-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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