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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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