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WIND-TUNNEL TESTS OF THE STATIC LONGITUDINAL CHARACTERISTICS AT LOW SPEED OF A SWEPT-WING AIRPLANE WITH BLOWING FLAPS AND LEADING-EDGE SLATSLow speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge slats
Document ID
19630003231
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
James, H. A. (NASA Ames Research Center Moffett Field, CA, United States)
Maki, R. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 1, 2013
Publication Date
April 5, 1957
Subject Category
Biosciences
Report/Patent Number
NACA-RM-A57D11
Report Number: NACA-RM-A57D11
Accession Number
63N13107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LEADING EDGE
AERODYNAMIC CHARACTERISTICS
FLAP
SWEPT WING

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