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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