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Flying qualities of a high-speed bomber with a dual pusher propeller aft of the empennage as estimated from wind-tunnel tests of a 1/8-scale powered model
Document ID
19930092595
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schnurbusch, Alfred W
Date Acquired
September 6, 2013
Publication Date
November 4, 1944
Report/Patent Number
NACA-MR-A4K04
NACA-WR-A-78
Report Number: NACA-MR-A4K04
Report Number: NACA-WR-A-78
Accession Number
93R21885
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SIDESLIPPING - DOUGLAS B-42
STABILITY & CONTROL - DOUGLAS B-42
ELEVATOR CONTROLS - DOUGLAS B-42
WIND TUNNEL TESTS - AAL - (10' X 7')
AIRPLANES - DOUGLAS B-42 (EXPERIMENTAL) WIND TUNNEL TESTS (AAL-7'X10') (AMER) AI

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