Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303

Author: Foster, Gerald V.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L55F06
Link: https://digital.library.unt.edu/ark:/67531/metadc61412/

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