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Results of a Rocket-model Investigation of Control-surface Buzz and Flutter on a 4-percent-thick Unswept Wing and on 6-, 9-, and 12-percent-thick Swept Wings at Transonic Speeds
Document ID
19930089146
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Henning, Allen B
Date Acquired
August 16, 2013
Publication Date
November 20, 1953
Report/Patent Number
NACA-RM-L53I29
Report Number: NACA-RM-L53I29
Accession Number
93R18436
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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