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Some effects of sweepback and airfoil thickness on longitudinal stability and control characteristics at transonic speedsInformation on the longitudinal stability and control characteristics of complete transonic airplane configurations is compiled in a form that might indicate whether or not a consistent pattern of behavior exists in regard to the effects of airfoil thickness and sweepback on overall stability and control characteristics at transonic speeds.
Document ID
19770022132
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Donlan, C. J. (NASA Langley Research Center Hampton, VA, United States)
Luoma, A. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Collected Works of Charles J. Donlan
Subject Category
Aircraft Stability And Control
Accession Number
77N29076
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19770022115Collected WorksCollected works of Charles J. Donlan
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