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Influence of Wing and Fuselage on the Vertical-tail Contribution to the Low-speed Rolling Derivatives of Midwing Airplane Models with 45 Degree Sweptback Surfaces
Document ID
19930083409
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wolhart, Walter D
Date Acquired
August 16, 2013
Publication Date
December 1, 1951
Report/Patent Number
NACA-TN-2587
Report Number: NACA-TN-2587
Accession Number
93R12699
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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