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Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)最新文献

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Design of Experiments for Expansion Tube Evaluation of Magnetohydrodynamic Aerobraking for Earth Return from Deep Space 深空返回地球磁流体动力航空制动膨胀管评价试验设计
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0207-cd
A. Lefevre, David E. Gildfind, Rowan J.Gollan, Peter A. Jacobs
In this paper a series of experiments are designed aiming to test the MHD aerobraking concept in an expansion tube, where the operating conditions are representative of a realistic Earth reentry flight condition. An expansion tube can generate the flow properties relevant to Earth reentry conditions, matching the associated velocity and density. These facilities can also ensure that ionization is confined to the shock layer, which is a major characteristic of a reentry flight, and which arcjet facilities cannot provide. In the first part of this paper several Earth return trajectories are considered, including Low Earth Orbit, Moon, Mars and Asteroid return missions. It was found that a significant MHD interaction can be expected to occur for a large portion of the studied trajectories, provided that the vehicle size and velocity is sufficient, which is true for most of these missions. In the second part, the flow processes that take place in an expansion tube are modeled analytically, using NASA’s CEA2 equilibrium chemistry solver, and with the Navier-Stokes flow solver, Eilmer4. It is shown that a suitable non-ionized freestream can be provided by UQ’s X2 and X3 facilities, along with a high MHD interaction, while matching real flight conditions from past Earth reentry missions. Two scaled reentry experiments are proposed, based on NASA’s Stardust, one in X2, the other one in X3. More detailed analysis with Eilmer4 shows that chemical non-equilibrium effects in the shock layer are significant, especially for the X3 condition, hence finite-rate chemistry will be needed to analyze these experiments.
本文设计了一系列实验,旨在测试MHD气动制动概念在膨胀管中,其操作条件代表了现实的地球再入飞行条件。膨胀管可以产生与地球再入条件相关的流动特性,匹配相应的速度和密度。这些设施还可以确保电离被限制在激波层,这是再入飞行的一个主要特征,而这是电弧喷射设施无法提供的。在本文的第一部分,考虑了几种地球返回轨道,包括近地轨道,月球,火星和小行星返回任务。研究发现,如果飞行器的尺寸和速度足够大,那么在研究的大部分轨迹中,可以预期会发生显著的MHD相互作用,这对大多数任务来说都是正确的。在第二部分中,使用NASA的CEA2平衡化学求解器和Navier-Stokes流动求解器Eilmer4,对膨胀管内发生的流动过程进行了解析建模。结果表明,UQ的X2和X3设备可以提供合适的非电离自由流,同时具有高MHD相互作用,同时符合过去地球再入任务的实际飞行条件。基于NASA的“星尘号”,计划进行两次规模再入实验,一次在X2,另一次在X3。用Eilmer4进行更详细的分析表明,激波层中的化学非平衡效应是显著的,特别是在X3条件下,因此需要用有限速率化学来分析这些实验。
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引用次数: 0
Experimental and Numerical Studies of Ultrasonic Cavitation-Assisted Ballast Water Treatment Process 超声空化辅助压载水处理过程的实验与数值研究
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0322-cd
X. Lu, Tandiono, C. Turangan, C. W. Kang, H. Osman, F. Lim, M. Lucas
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引用次数: 0
Shock-shock interactions in granular flows 颗粒流动中的激波-激波相互作用
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0344-cd
Shivam Verma, Aqib Khan, Priyanka Hankare, Rakesh Kumar, Sanjay Kumar
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引用次数: 0
Computational Studies on the Unsteadiness in Hypersonic Shock Induced Leading Edge Separation 高超声速激波前缘分离非定常计算研究
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0297-cd
S. K. Karthick, R. Sriram
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引用次数: 0
Effects of Urban Terrain on Spatial Distribution of Explosion Products 城市地形对爆炸产物空间分布的影响
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0021-cd
Azi Lipshtat, S. Pistinner
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引用次数: 0
Separation of Laminar Boundary Layers at Swept Corners 后掠角层流边界层的分离
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0324-cd
R. R. Pulimidi, F. Lu
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引用次数: 0
Preliminary Measurement of the Propagating Detonation Wave Velocity in the Circular Tube Induced by Combustion of Air-Acetylene Mixture Using Ion Probes 用离子探针初步测量空气-乙炔混合物燃烧引起的圆管内传播爆轰波速度
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0368-cd
S. Udagawa, Y. Suda, T. Inage, M. Ota, Y. Hirose
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引用次数: 0
Effect of Cross-Wire Tab Offset on Twin-Jet Mixing Characteristics 交叉丝片偏置对双射流混合特性的影响
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0131-cd
Dhruv Dwived, Aqib Khan, Rakesh Kumar, S. Ibrahim
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引用次数: 0
Discontinuous Galerkin Simulation of the Shock-vortex Interaction in Dusty Gas Shardin’s Problem 含尘气体Shardin问题中激波-涡相互作用的不连续Galerkin模拟
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0097-cd
O. Ejtehadi, A. Rahimi, R. Myong
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引用次数: 0
The Study of Radiation Characteristics of The rmo-che micalNonequilibrium Flow Field Using State-to-state Model 用状态-状态模型研究非平衡流场的辐射特性
Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0330-cd
Weijie Zheng, Ming-hua Zeng, Dongfang Wang, Zhenxia Chai, Shichao Zhe ng
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引用次数: 0
期刊
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)
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