Investigation of the aerodynamic characteristics of a model of a supersonic bomber configuration with a swept and an unswept wing at Mach numbers from 1.79 to 2.67

Author: Silvers, H. Norman
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L58C27
Link: https://digital.library.unt.edu/ark:/67531/metadc64207/

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