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An experimental investigation of reduction in transonic drag rise at zero lift by the addition of volume to the fuselage of a wing-body-tail configuration and a comparison with theory
Author:
Holdaway, George H.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A54F22
Link:
https://digital.library.unt.edu/ark:/67531/metadc62752/
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