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Free-flight Investigation of the Rolling Effectiveness of a Wing-spoiler Arrangement at High Subsonic, Transonic, and Supersonic Speeds
Document ID
19930085323
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sandahl, Carl A
Date Acquired
August 16, 2013
Publication Date
May 17, 1948
Report/Patent Number
NACA-RM-L8A07
Report Number: NACA-RM-L8A07
Accession Number
93R14613
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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