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Wing-flow Measurements of Longitudinal Stability and Control Characteristics of a Supersonic Airplane Configuration Having a 42.8 Degree Sweptback Circular Arc Wing with Aspect Ratio 4.0, Taper Ratio 0.50, and Sweptback Tail Surfaces
Document ID
19930086273
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Crane, Harold L
Adams, James J
Date Acquired
August 16, 2013
Publication Date
April 3, 1950
Report/Patent Number
NACA-RM-L50B09
Report Number: NACA-RM-L50B09
Accession Number
93R15563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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