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Effects of Propeller Operation and Angle of Yaw on the Distribution of the Load on the Horizontal Tail Surface of a Typical Pursuit AirplaneNo abstract available
Document ID
19930092859
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
Authors
Dingeldein, Richard C
Date Acquired
September 6, 2013
Publication Date
February 1, 1944
Subject Category
Aircraft Stability And Control
Report/Patent Number
NACA-ARR-4B10
NACA-WR-L-227
Report Number: NACA-ARR-4B10
Report Number: NACA-WR-L-227
Accession Number
93R22149
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TAIL SURFACES-CURTISS P-40K-WIND TUNNEL TESTS(NACA-FULL-SCALE)
AIRPLANES-CURTISS P-40K-WIND TUNNEL TESTS(NACA-FULL-SCALE)(AMER )
YAWING MOMENTS - TAIL SURFACES - CURTISS P-40K
AIR FLOW - TAIL SURFACES
PROPELLERS - OPERATION
DOWNWASH ANGLES
PRESSURE DISTRIBUTION - TAIL SURFACES - CURTISS P-40K
LOAD DISTRIBUTION - TAIL SURFACES - CURTISS P-40K
PULL-UPS - CURTISS P-40K

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