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Wind-Tunnel Tests of a Twin-engine Model to Determine the Effect of Direction of Propeller Rotation on the Static-Stability Characteristics
Document ID
19930092572
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Swanson, Robert S
Date Acquired
September 6, 2013
Publication Date
January 1, 1943
Report/Patent Number
NACA-WR-L-295
Report Number: NACA-WR-L-295
Accession Number
93R21862
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - TRIM
AIRPLANES, TWO-ENGINE
LIFT, DRAG & PITCHING MOMENTS - NORTH AMERICAN B-28
STABILITY, STATIC
STABILITY, DIRECTIONAL - NORTH AMERICAN B-28
STABILITY TESTS - NORTH AMERICAN B-28 WIND TUNNEL
PROPELLER SLIPSTREAM - EFFECT ON STABILITY
WING FLAPS, DUPLEX
PROPELLERS, TANDEM - WIND TUNNEL TESTS
PROPELLERS - PROPULSIVE EFFICIENCY

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