zou xiao-bing, wang xin-xin, luo cheng-mu, et al. Mach number measurement of the gas flow from the supersonic nozzle in gas puff Zpinch[J]. High Power Laser and Particle Beams, 2002, 14.
Citation:
zou xiao-bing, wang xin-xin, luo cheng-mu, et al. Mach number measurement of the gas flow from the supersonic nozzle in gas puff Zpinch[J]. High Power Laser and Particle Beams, 2002, 14.
zou xiao-bing, wang xin-xin, luo cheng-mu, et al. Mach number measurement of the gas flow from the supersonic nozzle in gas puff Zpinch[J]. High Power Laser and Particle Beams, 2002, 14.
Citation:
zou xiao-bing, wang xin-xin, luo cheng-mu, et al. Mach number measurement of the gas flow from the supersonic nozzle in gas puff Zpinch[J]. High Power Laser and Particle Beams, 2002, 14.
The Mach number of the gas flow from the supersonic nozzle in a gaspuff Zpinch was determined by the two pressure transducer method. The measured Mach number rises with time and reaches to a maximum value of 4.25 that is close to 4.8, the value from a steadystate gas flow calculation. This result shows that the steadystate gas flow calculation can be used to estimate the Mach number of gas flow from a supersonic nozzle in gas puff Zpinch.
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