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Flight Investigation of the Supersonic Area Rule for a Straight Wing-body Configuration at Mach Numbers Between 0.8 and 1.5
Document ID
19930088641
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoffman, Sherwood
Wolff, Austin L
Faget, Maxime A
Date Acquired
August 16, 2013
Publication Date
April 29, 1955
Report/Patent Number
NACA-RM-L55C09
Report Number: NACA-RM-L55C09
Accession Number
93R17931
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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