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STABILITY AND CONTROL CHARACTERISTICS AT SUBSONIC SPEEDS OF A FLAT-TOP ARROWHEAD WING-BODY COMBINATIONStability and control of flat surface wing- fuselage combination at subsonic speed - effect of wing leading edge sweepback
Document ID
19630004879
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Buell, D. A. (NASA Ames Research Center Moffett Field, CA, United States)
Johnson, N. S. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-3-5-59A
Accession Number
63N14755
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING-FUSELAGE COMBINATION
SUBSONIC SPEED
FLAT SURFACE
SWEPTBACK WING
STABILITY AND CONTROL
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