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Power-On Longitudinal-Stability and Control Tests of the 1/8-scale Model of the Brewster F2A Airplane Equipped with Full-Span Slotted Flaps and a New Horizontal Tail
Document ID
19930092608
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Toll, Thomas A
Date Acquired
September 6, 2013
Publication Date
March 1, 1942
Report/Patent Number
NACA-WR-L-709
Report Number: NACA-WR-L-709
Accession Number
93R21898
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING FLAPS, SLOTTED - FULL-SPAN
GROUND EFFECT
CENTER OF GRAVITY - POSITION
ELEVATORS - DEFLECTION
TAIL SURFACES, HORIZONTAL - BREWSTER F2A
STABILITY & CONTROL, LONGITUDINAL - BREWSTER F2A POWER-ON
AIRPLANES - BREWSTER F2A WIND TUNNEL TESTS (AMER )

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