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Aerodynamic Characteristics of a 1/8-scale Powered Model of a High-speed Bomber with a Dual Pusher Propeller Aft of the Empennage
Document ID
19930092682
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schnurbusch, Alfred W
Date Acquired
September 6, 2013
Publication Date
October 12, 1945
Report/Patent Number
NACA-MR-A5J12
NACA-WR-A-89
Report Number: NACA-MR-A5J12
Report Number: NACA-WR-A-89
Accession Number
93R21972
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GROUND EFFECT - WIND TUNNEL TESTS
STABILITY & CONTROL - DOUGLAS B-42
AIRPLANES - DOUGLAS B-42 (EXPERIMENTAL) WIND TUNNEL TESTS -AAL (10' X 7') (AMER
WIND TUNNEL TESTS - AAL (10'X 7')

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