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Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing fuselage combination having a triangular wing of aspect ratio 4
Document ID
19930087666
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fournier, Paul G
Date Acquired
August 29, 2013
Publication Date
August 28, 1953
Report/Patent Number
NACA-RM-L53G14a
Report Number: NACA-RM-L53G14a
Accession Number
93R16956
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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