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Small-scale investigation at transonic speeds of the effects of thickening the inboard section of a 45 degrees sweptback wing of aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section
Document ID
19930086892
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spreemann, Kenneth P
Alford, William J , Jr
Date Acquired
August 29, 2013
Publication Date
August 9, 1951
Report/Patent Number
NACA-RM-L51F08a
Report Number: NACA-RM-L51F08a
Accession Number
93R16182
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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