The longitudinal characteristics at Mach numbers up to 0.9 of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and an aspect ratio of 10

Author: Tinling, Bruce E.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A52I19
Link: https://digital.library.unt.edu/ark:/67531/metadc59448/

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