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The characteristics of the NACA M-12 airfoil sectionThe data obtained on the NACA M-12 airfoil, tested at twenty atmosphere density in the NACA variable density wind tunnel, have been extended by additional tests at one and at twenty atmospheres under improved conditions. The results of these tests are given. Considerable scale effect was found.
Document ID
19930081048
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Higgins, George J
Date Acquired
September 6, 2013
Publication Date
August 1, 1926
Report/Patent Number
NACA-TN-243
Report Number: NACA-TN-243
Accession Number
93R10338
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - CLARK Y - CHAR & C P
AIRFOILS - ANGLE OF ATTACK
AIRFOILS, N A C A - M6 CHAR & C P
AIRFOILS - NACA 997 - CHARACTERISTICS
AIRFOILS - CHARACTERISTICS

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