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The NACA CYH Airfoil SectionThe NACA CYH airfoil section is described and its aerodynamic characteristics are given as tested in the NACA variable density wind tunnel at twenty atmosphere pressure. This section has a low drag, a high maximum lift, and a small travel of center of pressure.
Document ID
19930081042
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Higgins, George J
Date Acquired
September 6, 2013
Publication Date
June 1, 1926
Report/Patent Number
NACA-TN-240
Report Number: NACA-TN-240
Accession Number
93R10332
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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