Effect of heat release on movement characteristics of shock train in an isolator
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Wen Bao | Juntao Chang | Wen Shi | Shuo Feng | Chenlin Zhang | MengMeng Liu | W. Bao | Chenlin Zhang | Shuo Feng | W. Shi | Jun-tao Chang | MengMeng Liu
[1] Zhenguo Wang,et al. Influences of H2O mass fraction and chemical kinetics mechanism on the turbulent diffusion combustion of H2–O2 in supersonic flows , 2012 .
[2] Nickolay Smirnov,et al. Accumulation of errors in numerical simulations of chemically reacting gas dynamics , 2015 .
[3] Karthik Duraisamy,et al. Large-Eddy Simulations of a normal shock train in a constant-area isolator , 2014 .
[4] M. Sun,et al. Flame Flashback in a Supersonic Combustor Fueled by Ethylene with Cavity Flameholder , 2015 .
[5] P. Sagaut,et al. Large-eddy simulation of the shock/boundary layer interaction , 2001 .
[6] Yoshiaki Miyazato,et al. Shock train and pseudo-shock phenomena in internal gas flows , 1999 .
[7] Hui-jun Tan,et al. Unstart of a Hypersonic Inlet with Side Compression Caused by Downstream Choking , 2016 .
[8] A. Hadjadj. Large-Eddy Simulation of Shock/Boundary-Layer Interaction , 2012 .
[9] C. Westbrook,et al. A comprehensive modeling study of hydrogen oxidation , 2004 .
[10] Jonathan S. Geerts,et al. Experimental Characterization of Isolator Shock Train Propagation , 2012 .
[11] He-xia Huang,et al. Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves , 2012 .
[12] H. Olivier,et al. Experimental Investigation of Wall and Total Temperature Influence on a Shock Train , 2014 .
[13] Nicholas J. Georgiadis,et al. Numerical Simulation of a Hydrogen-Fueled Dual-Mode Scramjet Engine Using Wind-US , 2009 .
[14] Ehsan Roohi,et al. Three dimensional investigation of the shock train structure in a convergent-divergent nozzle , 2014 .
[15] Daren Yu,et al. Backpressure unstart detection for a scramjet inlet based on information fusion , 2014 .
[16] Wei Huang,et al. Parametric effects on the combustion flow field of a typical strut-based scramjet combustor , 2011 .
[17] Zhang Yan,et al. Numerical Simulation of a Dual-Mode Scramjet Combustor Using Flamelet Scheme , 2014 .
[18] W. Su,et al. Effects of Dynamic Backpressure on Pseudoshock Oscillations in Scramjet Inlet-Isolator , 2016 .
[19] Jun-tao Chang,et al. Unstart Margin Characterization Method of Scramjet Considering Isolator–Combustor Interactions , 2015 .
[20] H. Tan,et al. Experimental Investigation of the Unstart Process of a Generic Hypersonic Inlet , 2011 .
[21] Michael Oevermann,et al. Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling , 2000 .
[22] Sebastian Karl,et al. Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor. Part II: Large eddy simulations , 2015 .
[23] Nickolay Smirnov,et al. Hydrogen fuel rocket engines simulation using LOGOS code , 2014 .
[24] J. Swithenbank. Hypersonic air-breathing propulsion , 1967 .
[25] M. Akella,et al. Unstart Detection in a Simplified-Geometry Hypersonic Inlet-Isolator Flow , 2010 .
[26] Daren Yu,et al. Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward Movement , 2016 .
[27] Jun Liu,et al. Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows , 2012 .
[28] Wei Shyy,et al. Adaptive Turbulent Schmidt Number Approach for Multi- Scale Simulation of Supersonic Crossflow , 2011 .
[29] Wei Huang,et al. Molecular weight and injector configuration effects on the transverse injection flow field properties in supersonic flows , 2014 .
[30] Ye Tian,et al. Experimental and numerical investigations of combustion mode transition in a direct–connect scramjet combustor , 2015 .
[31] Zhenguo Wang,et al. Theoretical analysis of flamelet model for supersonic turbulent combustion , 2012 .
[32] Matthew Fotia,et al. Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet–Scramjet Experiment , 2015 .
[33] Li Yan,et al. Numerical exploration of mixing and combustion in a dual-mode combustor with backward-facing steps , 2016 .
[34] Noor A. Ahmed,et al. Transient behavior of shock train with and without controlling , 2015 .
[35] Zhenwei Zhao,et al. An updated comprehensive kinetic model of hydrogen combustion , 2004 .
[36] Nickolay Smirnov,et al. Modeling and simulation of hydrogen combustion in engines , 2014 .
[37] Daniel B. Le,et al. Shock Train Leading-Edge Detection in a Dual-Mode Scramjet , 2008 .
[38] F. Menter. ZONAL TWO EQUATION k-w TURBULENCE MODELS FOR AERODYNAMIC FLOWS , 1993 .
[39] Jing Lei,et al. Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator , 2011 .