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Low-Speed Investigation Of The Effects Of Horizontal-Tail Area And Wing Sweep On The Static Longitudinal Stability And Control Characteristics Of An Airplane Configuration Having Tail Surfaces Outboard Of The Wing TipsLow-speed longitudinal static stability & control characteristics of aircraft with swept wings & tail surfaces outboard of wing tips
Document ID
19630010604
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Hayes, W. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Sleeman, W. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
June 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-6-11-59L
Accession Number
63N20484
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
LOW SPEED STABILITY
SWEPT WING
STATIC STABILITY AND CONTROL
LONGITUDINAL STABILITY AND CONTROL
TAIL SURFACE

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