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Some Effects of Spoiler Height, Wing Flexibility, and Wing Thickness on Rolling Effectiveness and Drag of Unswept Wings at Mach Numbers Between 0.4 and 1.7
Document ID
19930087247
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fields, E M
Date Acquired
August 16, 2013
Publication Date
October 7, 1952
Report/Patent Number
NACA-RM-L52H18
Report Number: NACA-RM-L52H18
Accession Number
93R16537
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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