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Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 2.46 and 3.36. The investigation includes some comparison of the effects of Mach number, Reynolds number, and thickening the wing root sections on the loading.
Document ID
19930088436
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kaattari, George E
Date Acquired
August 16, 2013
Publication Date
January 18, 1955
Report/Patent Number
NACA-RM-A54J12
Report Number: NACA-RM-A54J12
Accession Number
93R17726
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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