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Effects of wing leading-edge deflection on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configurationWing leading-edge deflection effects on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration were determined. Static force tests were conducted in a V/STOL tunnel at a Reynolds number of about 2.5 x 1 million for an angle-of-attack range from -10 deg to 17 deg and an angle-of-sideslip range from -5 deg to 5 deg. Limited flow visualization studies were also conducted in order to provide a qualitative assessment of leading-edge upwash characteristics.
Document ID
19780025104
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Coe, P. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Weston, R. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-78787
Accession Number
78N33047
Funding Number(s)
PROJECT: RTOP 743-04-13-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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