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Effect on Transonic and Supersonic Drag of a Fuselage Protuberance Designed to Improve the Area Distribution of an Essentially Unswept Wing-fuselage Combination
Document ID
19930088006
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sandahl, Carl A
Date Acquired
August 16, 2013
Publication Date
January 5, 1954
Report/Patent Number
NACA-RM-L53K10
Report Number: NACA-RM-L53K10
Accession Number
93R17296
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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