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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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