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Flight Tests of an All-movable Horizontal Tail with Geared Unbalancing Tabs on the Curtiss XP-42 Airplane
Document ID
19930081790
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kleckner, Harold F
Date Acquired
August 16, 2013
Publication Date
October 1, 1946
Report/Patent Number
NACA-TN-1139
Accession Number
93R11080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - CURTISS P-36A (AMER)
TAIL SURFACES, ALL-MOVABLE
CONTROL STICKS - FORCES, PILOT
ELEVATOR CONTROLS - CURTISS P-42
STABILITY & CONTROL, LONGITUDINAL - CURTISS P-42
TAIL SURFACES, HORIZONTAL - CURTISS P-42 FLIGHT TESTS
ELEVATORS - HINGE MOMENTS - CURTISS P-42
TABS - CURTISS P-36A (AMER )
SIDESLIPPING - CURTISS P-42

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