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Aerodynamic characteristics of a 68.4 degree delta wing at Mach numbers of 1.6 and 1.9 over a wide Reynolds number range
Author:
Hatch, John E , Jr
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53I08
Link:
https://digital.library.unt.edu/ark:/67531/metadc59872/
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