Aerodynamic characteristics of various configurations of a model of a 45 degree swept-wing airplane at a Mach number of 2.01

Author: Spearman, M. Leroy
Additional Authors: Driver, Cornelius
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54J08
Link: https://digital.library.unt.edu/ark:/67531/metadc64971/

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