Development and Validation of a Compressible Reacting Gas-Dynamic Flow Solver for Supersonic Combustion by Anvar Gilmanov, Ponnuthurai Gokulakrishnan, Michael S. Klassen

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Axisymmetric and three-dimensional flow simulation of a mixed compression supersonic air inlet by M. Abedi, R. Askari, J. Sepahi-Younsi, M.R. Soltani

“…The flow through an axisymmetric supersonic mixed-compression air inlet has been simulated numerically to investigate the effects and the necessity of the three-dimensional (3D) modeling in comparison with the axisymmetric one. …”
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Combustion Characteristics of a Supersonic Combustor with a Large Cavity Length-to-Depth Ratio by Xiang Li, Qingchun Lei, Xiaocun Zhao, Wei Fan, Shuang Chen, Li Chen, Ye Tian, Quan Zhou

“…The combustion characteristics of a hydrogen-fueled supersonic combustor featuring a large cavity length-to-depth ratio (i.e., 11) were examined by performing experimental trials while varying the fuel injector positions and equivalence ratios. …”
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A Mixing Process Influenced by Wall Jet-Induced Shock Waves in Supersonic Flow by Ji Zhang, Daoning Yang, Yi Wang, Dongdong Zhang

Subjects: “…supersonic mixing layer…”
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The Relationship between Contraction of the Ejector Mixing Chamber and Supersonic Jet Mixing Layer Development by Qi Jing, Wanwu Xu, Wei Ye, Zhiyan Li

“…Supersonic mixing layer development seriously impacts on the performance of an ejector, and the effect of mixing chamber contraction angle on supersonic jet mixing has been poorly studied. …”
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Impact of the convergent geometric profile on boundary layer separation in the supersonic over-expanded nozzle by Dehane Rabie, Naima Khatir, Liazid Abdelkrim, Inc Mustafa, Benarous Abdallah, Ahmad Hijaz, Menni Younes

“…The findings indicated that the convergent profile must be considered during the design phase when focusing on the problem of boundary layer separation in the supersonic overexpanded regime nozzles.…”
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Numerical Simulation of a Supersonic Ejector for Vacuum Generation with Explicit and Implicit Solver in Openfoam by Ll Macia, R. Castilla, P. J. Gamez-Montero, S. Camacho, E. Codina

Subjects: “…supersonic vacuum ejector…”
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Passive flow modification over the supersonic and the hypersonic air-intake system using bleed by Sinha Jayanta, Singh Sanjay, Prakash Om, Panchal Dhruv

“…The current research focuses on the numerical simulation of the supersonic and hypersonic air inlet and its starting and unstarting characteristics. 2D RANS equation for supersonic and hypersonic intake has been solved using the k-oSST turbulence model. …”
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Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design by Sihmehmet Yildiz, Hayriye Pehlivan Solak, Melike Nikbay

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Research Progress of Supersonic Jet Mixing Enhancement Technology Based on Slope and Wavy Wall by Wang Ruorong, Guo Zhenyun, Huang Wei

“…Therefore, the mixing enhancement strategy of supersonic fuel has gradually become a research focus of aerospace scholars at home and abroad. …”
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Comparative Analysis of Pressure Swing Adsorption and Supersonic Separators for High-Purity Hydrogen Applications by Leonardo O.S. Santana, Gustavo S. Santos, Artur S. Bispo, Chrislaine B. Marinho, Victor L.S. Dias, Ana L.N. Santos, Jade S. Avila, Fernando L.P. Pessoa

“…Compared with traditional processing, the main advantage of supersonic separation technology is its small size and flexible structure. …”
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Controlling the flow loss of a supersonic compressor rotor using the blade slotting method by Xinlong Ye, Zhenggui Zhou

“…The flow loss in the blade passage of a supersonic compressor rotor mainly comes from the boundary layers on the blade surface and end wall, the shock wave, the shock wave/boundary layer interaction, and tip leakage flow; the instability is mainly caused by the shock wave near the rotor blade tip exiting the blade passage. …”
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Numerical research on flow field starting of supersonic compressor in outlet-opening wind tunnel by ZHANG Tianlong, WANG Xu, LIN Tianqi, XU Xiangshen, MU Wenpeng

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Experimental and Numerical Investigations on the Mixing Process of Supercritical Jet Injected into a Supersonic Crossflow by Wenyuan Zhou, Kai Xing, Suyi Dou, Qingchun Yang, Xu Xu

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Aerodynamic Study on the Influence Mechanism of Bow Blades on the Flow Field of Supersonic Tandem Rotors by Hao Cheng, Zhaoyun Song, Bo Liu

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Dynamics of supersonic microparticle impact on elastomers revealed by real–time multi–frame imaging by Veysset, David Georges, Maznev, Alexei, Masser, Kevin A., Nelson, Keith Adam, Hsieh, Alex J, Kooi, Steven E

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The Supersonic Project: Shining Light on SIGOs—A New Formation Channel for Globular Clusters by Chiou, Yeou S, Naoz, Smadar, Burkhart, Blakesley, Marinacci, Federico, Vogelsberger, Mark

“…All rights reserved. Supersonically induced gas objects (SIGOs) with little to no dark matter (DM) component are predicted to exist in patches of the universe with non-negligible relative velocity between baryons and the DM at the time of recombination. …”
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A Quantitative Assessment of Advanced Take-off Trajectories for Supersonic Transport Noise Reduction by Voet, Laurens Jozef Amandine

“…This thesis (a) establishes the design trades and limitations of supersonic transport propulsion systems in terms of take-off noise reduction, (b) identifies the attributes, quantifies the potential, and assesses the impact of advanced take-off trajectories designed for noise reduction, and (c) formulates a reduced-order model to scale these results for supersonic transport of different size classes and cruise Mach numbers. …”
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A comparative study on the use of calibrated and rainbow schlieren techniques in axisymmetric supersonic jets by Mariani, Raffaello, Zang, Bin, Lim, H. D., Vevek, U. S., New, Daniel Tze How, Cui, Y. D.

“…Detailed experimental comparisons had been conducted between calibrated and rainbow schlieren on perfectly- and under-expanded axisymmetric supersonic jets through a modified Z-type schlieren system. …”
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Influence of oncoming flow parameters on rotating detonation combustor with supersonic turbine guide vanes by Wen, Fengbo, Su, Liangjun, Wang, Ying, Han, Jiajun, Wang, Songtao

“…Therefore, the study of the influence of oncoming flow parameters on the coupling between the rotating detonation combustor and the supersonic turbine plays a key role in the design of the rotating detonation supersonic turbine engine. …”
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