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Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications
Document ID
19930092510
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Goranson, R Fabian
Date Acquired
September 6, 2013
Publication Date
July 1, 1942
Report/Patent Number
NACA-WR-L-392
Report Number: NACA-WR-L-392
Accession Number
93R21800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILIZERS
TAIL SURFACES, HORIZONTAL
WING FLAPS - FOWLER
AIRPLANES, FIGHTER
CENTER OF GRAVITY - POSITION
WING FLAPS, SLOTTED - FULL-SPAN
STABILITY & CONTROL, LONGITUDINAL
ELEVATORS - DEFLECTION

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