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An Investigation of the Effects of Jet Exhaust and Reynolds Number upon the Flow over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41
Document ID
19930088297
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Grigsby, Carl E
Date Acquired
August 16, 2013
Publication Date
June 17, 1954
Report/Patent Number
NACA-RM-L54E03
Report Number: NACA-RM-L54E03
Accession Number
93R17587
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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