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Some Effects of Aeroelasticity and Sweepback on the Rolling Effectiveness and Drag of a 1/11-scale Model of the Bell X-5 Airplane Wing at Mach Numbers from 0.6 to 1.5
Document ID
19930081603
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
English, Roland D
Date Acquired
August 16, 2013
Publication Date
November 18, 1953
Report/Patent Number
NACA-RM-L53I18b
Report Number: NACA-RM-L53I18b
Accession Number
93R10893
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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