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Wings with Variable Camber and SlotsInvestigations with a view to increasing the lift coefficient of a wing, without greatly increasing the C(sub x min), are chiefly related to the important question of the maximum speed range.
Document ID
20150020405
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lacaine, J.
(National Advisory Committee for Aeronautics Washington, DC, United States)
Date Acquired
November 3, 2015
Publication Date
August 1, 1933
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA Misc. Paper No. 37
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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