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Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 1.45 and 1.97Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 1.45 and 1.97. The investigation includes some comparison of the effects of Reynolds number and of thickening the wing root sections on the loading.
Document ID
19930088244
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kaattari, George E
Date Acquired
August 16, 2013
Publication Date
June 25, 1954
Report/Patent Number
NACA-RM-A54D19
Accession Number
93R17534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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