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Free-flight measurements of some effects of spoiler span and projection and wing flexibility on rolling effectiveness and drag of plain spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.6
Document ID
19930087271
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schult, Eugene D
Fields, E M
Date Acquired
August 29, 2013
Publication Date
October 3, 1952
Report/Patent Number
NACA-RM-L52H06a
Report Number: NACA-RM-L52H06a
Accession Number
93R16561
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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