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Effects of compressibility on maximum lift coefficients for six propeller airfoils
Document ID
19930092733
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cleary, Harold E
Date Acquired
September 6, 2013
Publication Date
January 1, 1945
Report/Patent Number
NACA-WR-L-514
NACA-ACR-L4L21a
Report Number: NACA-WR-L-514
Report Number: NACA-ACR-L4L21a
Accession Number
93R22023
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION - AIRFOILS - NACA 16-515
AIRFOILS - NACA 16-515 - CHARACTERISTICS PROPELLER
WIND TUNNEL TESTS (NACA-HIGH-SPEED-8')
PRESSURE DISTRITUTION - AIRFOILS - NACA 16-715
AIRFOILS - NACA 16-509 - CHARACTERISTICS PROPELLER
AIRFOILS, CAMBERED - CHARACTERISTICS
AIRFOILS - NACA 16-715 - CHARACTERISTICS PROPELLER
AIRFOILS - NACA16-709 - CHARACTERISTICS PROPELLER
PRESSURE DISTRIBUTION - AIRFOILS - NACA 16-215
AIRFOILS - NACA 16-209 - CHARACTERISTICS PROPELLER

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