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Experimental and theoretical aerodynamic characteristics of two low-aspect-ratio delta wings at angles of attack to 50 degrees at a Mach number of 4.07
Author:
Smith, Fred M
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57E02
Link:
https://digital.library.unt.edu/ark:/67531/metadc63854/
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