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WIND-TUNNEL INVESTIGATION OF DEVICES TO IMPROVE STATIC DIRECTIONAL STABILITY OF AN UNSWEPT-WING AIRPLANE MODEL AT MACH NUMBERS FROM 0.8 TO 2.2Wind tunnel tests to improve static directional stability of unswept-wing aircraft at mach 0.8-2.2
Document ID
19630004008
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Holtzclaw, R. W. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1958
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-MEMO-10-4-58A
Report Number: NASA-MEMO-10-4-58A
Accession Number
63N13884
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DIRECTIONAL STABILITY
TRANSONIC SPEED
UNSWEPT WING
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