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Free-Flight-tunnel Investigation of the Effect of Mode of Propeller Rotation Uuon the Lateral-stability Characteristics of a Twin-engine Airplane Model with Single Vertical Tails of Different Size
Document ID
19930092563
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pitkin, Marvin
Date Acquired
September 6, 2013
Publication Date
October 1, 1943
Report/Patent Number
NACA-ARR-3J18
NACA-WR-L-354
Report Number: NACA-ARR-3J18
Report Number: NACA-WR-L-354
Accession Number
93R21853
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INSTABILITY, SPIRAL
WING FLAPS, SLOTTED-PARTIAL-SPAN
PROPELLERS - ROTATION
PROPELLER SLIPSTREAM - EFFECT ON STABILITY
WING FLAPS - DEFLECTION
TAIL SURFACES, VERTICAL-TWO-ENGINE AIRPLANES
AIRPLANES, TWO-ENGINE
AIRPLANES, BOMBING - WIND TUNNEL TESTS
AIR FLOW - TAIL SURFACES
STABILITY & CONTROL, LATERAL

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