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Aerodynamic characteristics of a 60 degree delta wing having a half-delta tip control at a Mach number of 4.04
Author:
Ulmann, Edward F
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55A19
Link:
https://digital.library.unt.edu/ark:/67531/metadc61308/
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