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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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