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A fuselage addition to increase drag-rise Mach number of subsonic airplanes at lifting conditions
Author:
Whitcomb, Richard T.
Year:
1958
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-4290
Link:
https://digital.library.unt.edu/ark:/67531/metadc57155/
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