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Effects of Increasing Reynolds Number from 2 x 10(exp 6) to 6 x 10(exp 6) on the Aerodynamic Characteristics at Transonic Speeds of a 45 Degree Swept Wing with 6 Degree Leading-edge Droop
Document ID
19930088592
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schmeer, James W
Cooper, J Lawrence
Date Acquired
August 16, 2013
Publication Date
January 1, 1955
Report/Patent Number
NACA-RM-L54L10
Report Number: NACA-RM-L54L10
Accession Number
93R17882
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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