The effect of body contouring on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail and several wing-fuselage combinations having sweptback wings of relatively high aspect ratio

Author: Sutton, Fred B
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A56J08
Link: https://digital.library.unt.edu/ark:/67531/metadc64379/

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