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Calculation of the Aileron and Elevator Stick Forces and Rudder Pedal Forces for the Bell XP-83 Airplane (Project MX-511) in Spins
Document ID
19930092899
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schneiter, Leslie E
Date Acquired
September 6, 2013
Publication Date
September 1, 1945
Report/Patent Number
NACA-WR-L-575
NACA-MR-L5H29
Report Number: NACA-WR-L-575
Report Number: NACA-MR-L5H29
Accession Number
93R22189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL STICKS - FORCES
WIND TUNNEL TESTS - NACA - FREE-SPINNING (20')
WIND TUNNEL TESTS - NACA (6'X4')
CONTROL SURFACES - BELL P-83-WIND TUNNEL TESTS (NACA-6'X4' & FREE-SPINNING-2
SPINNING TESTS - BELL P-83-WIND TUNNEL (NACA-6'X4'& FREE-SPINNING- 20')

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