首页> 外文会议>10th IIR-Gustav Lorentzen conference on natural working fluids >SIMULATION OF SHOCK WAVES IN SUPERSONIC FLOW OF CO_2 THROUGH A CONVERGING-DIVERGING NOZZLE OF TRANSCRITICAL EJECTOR REFRIGERATION SYSTEM
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SIMULATION OF SHOCK WAVES IN SUPERSONIC FLOW OF CO_2 THROUGH A CONVERGING-DIVERGING NOZZLE OF TRANSCRITICAL EJECTOR REFRIGERATION SYSTEM

机译:跨喷头制冷系统汇流-扩散喷嘴在CO_2超音速流动中的激波模拟

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Shock waves in nonequilibrium liquid-vapor flow in a converging-diverging nozzle were simulated andrncompared to the experimental results in previous studies of the authors. Additional findings from simulationrnin the present study were found to be in agreement with the experimental results.rnIn the simulation, flow of uniformly dispersed droplets and vapor was assumed. Momentum and thermalrnrelaxation phenomena were incorporated in the derived equations. Simulation results using the equations forrnsupersonic two-phase flow of CO_2 in converging-diverging nozzles intended for a research on therntranscritical ejector refrigeration system are presented.rnIn a first previous study by the authors, shock waves along the diverging sections of relatively long nozzlesrnwere investigated in a blowdown device. Inlet conditions near the critical point were selected, wherein thernpressure range was 8–9 MPa and the obtained temperature range was 25–41℃. Correspondingly, backrnpressures ranged from 1.2 to 4.2 Mpa. In a second study by the authors, the expansion valve of the vaporrncompression refrigerator used was replaced by a relatively short converging-diverging nozzle to isolate thernnozzle and to easily investigate its inlet and outlet states. The inlet conditions used were 9–11 Mpa at 37–rn55℃. To determine different intensities of shock waves, the widest possible back-pressure range obtainedrnwas 3.6–5.9 Mpa.rnRelaxation phenomena, weak pseudo-shock waves and dispersed shock waves were obtained from thernsimulation. Weak pseudo-shock waves occurred in liquid-dominated two-phase flow, while dispersed shockrnwaves occurred in vapor-dominated flow. It was simulated and verified in this study that shock wavesrnintensify with increasing divergence angle given the same inlet condition, and with increasing supercriticalrninlet entropy given the same nozzle. The results are in agreement with the experiment and similar simulationrnresults in the previous studies.
机译:笔者对以往的研究结果进行了模拟,并模拟了在收敛-发散喷嘴中非平衡液体-蒸气流中的冲击波。在本研究中,从模拟中获得的其他发现与实验结果相符。在模拟中,假定了均匀分散的液滴和蒸气的流动。动量和热松弛现象被合并到导出的方程中。提出了使用CO_2超音速两相流在会聚-发散喷嘴中的方程进行模拟的结果,旨在用于跨临界喷射器制冷系统的研究。在作者的先前研究中,研究了沿较长喷嘴的发散段的冲击波。排污装置。选择接近临界点的入口条件,其中压力范围为8–9 MPa,获得的温度范围为25–41℃。相应地,背压范围为1.2至4.2Mpa。在作者的第二项研究中,所用的蒸气压缩式制冷机的膨胀阀被一个相对较短的会聚-发散喷嘴所代替,以隔离喷嘴,并易于研究其入口和出口状态。入口条件在37–55℃下为9-11 Mpa。为了确定不同强度的冲击波,从模拟中获得了最大的可能的背压范围,范围为3.6-5.9 Mpa。放松现象,较弱的伪冲击波和分散的冲击波被获得。在以液相为主的两相流中产生了较弱的拟激波,而在以气相为主的流中则出现了分散的冲击波。在本研究中进行了仿真和验证,在相同的进气条件下,冲击波随着发散角的增大而增强,在相同的喷嘴条件下,超临界进气口的熵增大。结果与实验结果和以前的研究结果相似。

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