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Study of the interaction of supersonic jets(Supersonic jet interaction for hypersonic flow of Mach 7. 1 and for variable Mach number, noting jet instability, stagnation pressure, drag variation, wind tunnel, etc)
Longitudinal aerodynamic characteristics at Mach numbers from 0. 50 to 1. 19 of a supersonic transport model with a modified M wing(Longitudinal aerodynamic characteristics at Mach numbers 0. 50 to 1. 19 of supersonic transport model with modified M wing)