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Low-speed Investigation of High-lift and Lateral Control Devices on a Semispan Variable-sweep Wing Having an Outboard Pivot LocationLeading edge and trailing edge flap deflection effect on high left and lateral control characteristics of semispan variable sweep wing and tail surfaces
Document ID
19650014317
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hammond, A. D. (NASA Langley Research Center Hampton, VA, United States)
Henderson, W. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-542
Report Number: NASA-TM-X-542
Accession Number
65N23918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LATERAL CONTROL
VARIABLE SWEEP
TRAILING-EDGE FLAP
LEADING-EDGE FLAP

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