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EFFECTS OF WING-CRANK, LEADING-EDGE CHORD EXTENSIONS AND HORIZONTAL-TAIL HEIGHT ON THE LONGITUDINAL STABILITY OF SWEPTWING MODELS AT MACH NUMBERS FROM 0.6 TO 1.4Effects of wing-crank, leading-edge chord extensions & horizontal-tail height on longitudinal stability of swept-wing models
Document ID
19630003104
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wakefield, R. M. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-92
Accession Number
63N12980
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC STABILITY
TAIL
LEADING EDGE
SWEPT WING
WING PLANFORM

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