Gust-Tunnel Investigation of the Effect of Leading Edge Separation on the Normal Accelerations Experienced by a 45 Degree Sweptback-Wing Model in Gusts

Author: Cahen, George L.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L53J07
Link: https://digital.library.unt.edu/ark:/67531/metadc59940/

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