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Experimental Determination at Subsonic Speeds of the Oscillatory and Static Lateral Stability Derivatives of a Series of Delta Wings with Leading-edge Sweep from 30 Degrees to 86.5 Degrees
Document ID
19930089516
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Letko, William
Date Acquired
August 16, 2013
Publication Date
April 12, 1957
Report/Patent Number
NACA-RM-L57A30
Report Number: NACA-RM-L57A30
Accession Number
93R18806
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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