Effect of boundary layer thickness on supersonic combustion in a scramjet combustor
暂无分享,去创建一个
Peibo Li | Jiajian Zhu | Yansong Li | Guo-yan Zhao | Yixin Yang | Fan Li | Yuhui Huang | Guangwei Ma | Ming-Chien Sun | Daoning Yang
[1] Guo-yan Zhao,et al. Effects of injection on flame flashback in supersonic crossflow , 2021, Aerospace Science and Technology.
[2] Hong-bo Wang,et al. Numerical investigation of the scale effects of the flame flashback phenomenon in scramjet combustors , 2021, Aerospace Science and Technology.
[3] Hong-bo Wang,et al. Scale effect of gas injection into a supersonic crossflow , 2021 .
[4] Ye Tian,et al. Investigation of combustion characteristics in a hydrogen-fueled scramjet combustor , 2021 .
[5] Hong-bo Wang,et al. Scaling effects on combustion modes in a single-side expansion kerosene-fueled scramjet combustor , 2021 .
[6] Ye Tian,et al. Pilot hydrogen enhanced combustion in an ethylene-fueled scramjet combustor at Mach 4 , 2021 .
[7] Hong-bo Wang,et al. Efficient WENOCU4 scheme with three different adaptive switches , 2020, Journal of Zhejiang University-SCIENCE A.
[8] Richard J. Thompson,et al. Numerical simulations of high frequency transverse pulsed jet injection into a supersonic crossflow , 2020 .
[9] Shun-hua Yang,et al. Investigation of Combustion Characteristics in a Kerosene-Fueled Supersonic Combustor with Air Throttling , 2020 .
[10] Guo-yan Zhao,et al. Effect of Injection Mach Number on Penetration in a Supersonic Crossflow , 2020 .
[11] M. Sun,et al. Numerical study of flow structures and mixing characteristics of a sonic jet in supersonic crossflow , 2020 .
[12] Ziao Wang,et al. Flame propagation and flashback characteristics in a kerosene fueled supersonic combustor equipped with strut/wall combined fuel injectors , 2019, Aerospace Science and Technology.
[13] Liang Li,et al. An Efficient Adaptive Central-Upwind WENO-CU6 Numerical Scheme with a New Sensor , 2019, Journal of Scientific Computing.
[14] M. Sun,et al. Investigation of flame flashback phenomenon in a supersonic crossflow with ethylene injection upstream of cavity flameholder , 2019, Aerospace Science and Technology.
[15] T. Rossmann,et al. Effect of boundary layer thickness on transverse sonic jet mixing in a supersonic turbulent crossflow , 2018, Physics of Fluids.
[16] Daren Yu,et al. Research progress on strut-equipped supersonic combustors for scramjet application , 2018, Progress in Aerospace Sciences.
[17] Hong-bo Wang,et al. Investigations of injection parameters on combustion oscillation in a supersonic crossflow , 2018, Acta Astronautica.
[18] Zun Cai,et al. Effect of cavity geometry on fuel transport and mixing processes in a scramjet combustor , 2018, Aerospace Science and Technology.
[19] Ye Tian,et al. Experimental study on the effect of equivalence ratio and injector position on flow structure and flame development in the scramjet combustor , 2018, Aerospace Science and Technology.
[20] Hongbo Wang,et al. Numerical dissipation control in an adaptive WCNS with a new smoothness indicator , 2018, Appl. Math. Comput..
[21] M. Sun,et al. Investigation of combustion characteristics in a scramjet combustor using a modified flamelet model , 2018 .
[22] Jun-tao Chang,et al. Local and global flame characteristics in a liquid kerosene fueled supersonic combustor equipped with a thin strut , 2018 .
[23] Krishna Murari Pandey,et al. Effect of variation of length-to-depth ratio and Mach number on the performance of a typical double cavity scramjet combustor , 2016 .
[24] Hong-bo Wang,et al. A flamelet model for supersonic non-premixed combustion with pressure variation , 2015 .
[25] Zhenguo Wang,et al. Analysis and modeling of blowout limits of cavity flame in supersonic flows , 2014 .
[26] Zhuyin Ren,et al. Partially premixed flamelet modeling in a hydrogen-fueled supersonic combustor , 2014 .
[27] A. Trebs. Ramp Injector Scale Effects on Supersonic Combustion , 2014 .
[28] Zhenguo Wang,et al. Numerical study on supersonic mixing and combustion with hydrogen injection upstream of a cavity flameholder , 2014 .
[29] S. Raghunathan,et al. An assessment of Scale Effects on Boundary Layer Transition on Natural Laminar Flow Nacelles , 2014 .
[30] Ning Qin,et al. Large-Eddy/Reynolds-averaged Navier–Stokes simulation of combustion oscillations in a cavity-based supersonic combustor , 2013 .
[31] Ning Qin,et al. Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder , 2013 .
[32] X. Bai,et al. Flame stabilization in a supersonic combustor with hydrogen injection upstream of cavity flame holders: experiments and simulations , 2011 .
[33] Jacqueline H. Chen,et al. Effects of Damköhler number on flame extinction and reignition in turbulent non-premixed flames using DNS , 2011 .
[34] B. Şahin,et al. Experimental measurement of flow past cavities of different shapes , 2010 .
[35] J. Driscoll,et al. Blowout Limits of Flames in High-Speed Airflows: Critical Damkohler Number , 2008 .
[36] Johan Steelant,et al. CFD Investigation of Scaling Laws for Hydrogen Fuelled Scramjet Combustors , 2008 .
[37] C. Law,et al. The effect of flame structure on soot formation and transport in turbulent nonpremixed flames using direct numerical simulation , 2007 .
[38] Corin Segal,et al. Penetration of Gaseous Jets In Supersonic Flows , 2006 .
[39] James F. Driscoll,et al. Correlation and Analysis of Blowout Limits of Flames in High-Speed Airflows , 2005 .
[40] R. Bowersox,et al. Stirred Reactor Analysis of Cavity Flame Holders for Scramjets , 1997 .
[41] D. G. Mabey,et al. A review of scale effects in unsteady aerodynamics , 1991 .
[42] Glenn S. Diskin,et al. Effects of scale on supersonic combustor performance , 1987 .
[43] Akira Yoshizawa,et al. A Statistically-Derived Subgrid-Scale Kinetic Energy Model for the Large-Eddy Simulation of Turbulent Flows , 1985 .
[44] N. Peters. Laminar diffusion flamelet models in non-premixed turbulent combustion , 1984 .
[45] T. Brooks,et al. Airfoil self noise - Effect of scale , 1983 .
[46] D. George-Falvy. Scale effect studies of airfoil profile drag at high subsonic speed , 1971 .