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Effects of wing-leading-edge modifications on a full-scale, low-wing general aviation airplane: Wind-tunnel investigation of high-angle-of-attack aerodynamic characteristicsWing-leading-edge modifications included leading-edge droop and slat configurations having full-span, partial-span, or segmented arrangements. Other devices included wing-chord extensions, fences, and leading-edge stall strips. Good correlation was apparent between the results of wind-tunnel data and the results of flight tests, on the basis of autorotational stability criterion, for a wide range of wing-leading-edge modifications.
Document ID
19820018341
Document Type
Technical Publication (TP)
Authors
Newsom, W. A., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Satran, D. R.
(NASA Langley Research Center Hampton, VA, United States)
Johnson, J. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1982
Subject Category
Aeronautics (General)
Report/Patent Number
L-15101
NASA-TP-2011
NAS 1.60:2011
Funding Number(s)
PROJECT: RTOP 505-41-13-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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