Research Article

The Principal Aspects of Application of Detonation in Propulsion Systems

Figure 20

The critical (lowest) Mach number for excitation of a detonation at interaction of an incident SW with various reflectors: identical mixture conditions and variation of SW Mach number for individual reflector. The area from the right of vertical line corresponds to successful initiation (“go”, “yes”), from the left to unsuccessful initiation (“no go”).
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