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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