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The Effect of Nacelle Location on the Zero-lift Drags of 45 Degree Sweptback Wing-body Configurations Having Boattail and Cylindrical Afterbodies as Determined by Flight Tests at Transonic Speeds
Document ID
19930088159
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoffmann, Sherwood
Wolff, Austin L
Date Acquired
August 16, 2013
Publication Date
March 25, 1954
Report/Patent Number
NACA-RM-L54B02
Report Number: NACA-RM-L54B02
Accession Number
93R17449
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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