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Effect of Airfoil Profile of Symmetrical Sections on the Low-speed Static-stability and Yawing Derivatives of 45 Degrees Sweptback Wing Models of Aspect Ratio 2.61
Document ID
19930085555
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Letko, William
Jaquet, Byron M
Date Acquired
August 16, 2013
Publication Date
November 9, 1948
Report/Patent Number
NACA-RM-L8H10
Report Number: NACA-RM-L8H10
Accession Number
93R14845
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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