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Flight measurements of compressibility effects on a three-blade thin Clark Y propeller operating at constant advance-diameter ratio and blade angle
Document ID
19930093326
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Vogeley, A W
Date Acquired
September 6, 2013
Publication Date
July 1, 1943
Report/Patent Number
NACA-ACR-3G12
NACA-WR-L-505
Report Number: NACA-ACR-3G12
Report Number: NACA-WR-L-505
Accession Number
93R22616
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPELLER THRUST & TORQUE
PROPELLERS - EFFICIENCY
PROPELLERS, THREE-BLADE
PROPELLERS - NACA 10-408-03RCY
AIRFOILS - CLARK Y PROPELLER
PROPELLERS - CHARACTERISTICS - EFFECT OF COMPRESSIBILITY
PROPELLERS, HIGH-SPEED - CHARACTERISTICS FLIGHT TESTS
MACH NUMNBER
INSTRUMENTS - THRUSTMETERS
AIRPLANES - BELL P-39 FLIGHT TESTS (EXPERIMENTAL) (AMER )

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