The effect of leading-edge extensions on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail combination having a 40 degree sweptback wing with NACA 64A thickness distribution

Author: Sutton, Fred B
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A55I29
Link: https://digital.library.unt.edu/ark:/67531/metadc61744/

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