高度未膨胀的稀薄射流

IF 2 Q2 ENGINEERING, MECHANICAL Frontiers in Mechanical Engineering Pub Date : 2023-08-09 DOI:10.3389/fmech.2023.1216927
N. Y. Bykov, Y. Gorbachev, S. Fyodorov
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引用次数: 0

摘要

计算研究了跃迁和散射状态下高度欠膨胀射流向背景的流出。采用直接模拟蒙特卡罗方法和Navier-Stokes方程。分析了主要参数对射流的影响。结果表明,在相对较窄的雷诺数范围内(5≤ReL≤30)发生剧烈的流动结构转变,表现为射流与周围气体的相互作用。在ReL = 5时,典型的欠膨胀射流激波结构完全退化。现有的经验表达式用于估计过渡区激波结构的特征尺寸,存在很大的不准确性。在考虑的参数范围内,基于直接模拟蒙特卡罗方法和基于Navier-Stokes (NS)方程解的方法在喷嘴区域得到了相似的结果,该区域的流动形式为流体动力。然而,使用NS方法评估稀薄激波层内的流动参数是有争议的。
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Highly underexpanded rarefied jet flows
A highly underexpanded jet outflow into the background in transition and scattering regimes is studied computationally. The direct simulation Monte Carlo method and Navier–Stokes equations are used. The main parameters’ impact on the jet flow is analyzed. It is shown that a drastic flow structure transformation occurs in a relatively narrow Reynolds numbers’ range, 5 ≤ ReL ≤ 30, featuring the jet–surrounding gas interaction. At ReL = 5, a shock wave structure that is typical for the underexpanded jet degenerates completely. The existing empirical expressions application for the estimation of the characteristic dimensions of the shock wave structure in the transition regime leads to significant inaccuracy. For the considered parameters’ range, the approaches based on the direct simulation Monte Carlo method and Navier–Stokes (NS) equations’ solution lead to similar results in the nozzle region, where the flow regime is hydrodynamic. Nevertheless, the NS approach employment for the assessment of flow parameters within rarefied shock layers is debatable.
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来源期刊
Frontiers in Mechanical Engineering
Frontiers in Mechanical Engineering Engineering-Industrial and Manufacturing Engineering
CiteScore
4.40
自引率
0.00%
发文量
115
审稿时长
14 weeks
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