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Effect of Leading-edge High-lift Devices and Split Flaps on the Maximum-lift and Lateral Characteristics of a Rectangular Wing of Aspect Ratio 3.4 with Circular-arc Airfoil Sections at Reynolds Numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6).
Document ID
19930085421
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lange, Roy H
May, Ralph W , Jr
Date Acquired
August 16, 2013
Publication Date
November 10, 1948
Report/Patent Number
NACA-RM-L8D30
Report Number: NACA-RM-L8D30
Accession Number
93R14711
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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