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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
Author:
Henning, Allen B
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53I29
Link:
https://digital.library.unt.edu/ark:/67531/metadc62228/
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