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Investigation of a Triangular Wing in Conjunction with a Fuselage and Horizontal Tail to Determine Downwash and Longitudinal-stability Characteristics : Transonic Bump Method
Document ID
19930086898
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Allen, Edwin C
Date Acquired
August 16, 2013
Publication Date
August 17, 1951
Report/Patent Number
NACA-RM-A51F12a
Report Number: NACA-RM-A51F12a
Accession Number
93R16188
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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