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Summary of Some Rocket-model Investigations of Effects of Wing Aspect Ratio and Thickness on Aileron Rolling Effectiveness Including Some Effects of Spanwise Aileron Location for Sweptback Wings with Aspect Ratio of 8.0
Document ID
19930088106
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Strass, H Kurt
Date Acquired
August 16, 2013
Publication Date
February 17, 1954
Report/Patent Number
NACA-RM-L53L11
Report Number: NACA-RM-L53L11
Accession Number
93R17396
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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