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Characteristics of swept wings at high speeds, 30 January 1952Some results of recent swept wing investigations are presented, that were undertaken to determine the effects of thickness and thickness distribution, camber and twist, nose-flap deflection, and devices or fixes for improving the wing pitching moment characteristics at high lift coefficients.
Document ID
19770022134
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Donlan, C. J. (NASA Langley Research Center Hampton, VA, United States)
Weil, J. (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 Design, Testing And Performance
Report/Patent Number
L52A15
Accession Number
77N29078
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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