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Thermal auto-ignition in high-speed droplet-laden mixing layers Ren ZX, Wang B, Xie QF, Wang DL Fuel, 191, 176, 2017 |
2 |
Parametric effect on the flow and mixing properties of transverse gaseous injection flow fields with streamwise slot: A numerical study Huang W, Li LQ, Chen XQ, Yan L International Journal of Hydrogen Energy, 42(2), 1252, 2017 |
3 |
Numerical investigation of H-2/air combustion instability driven by large scale vortex in supersonic mixing layers Qian C, Bing W, Zhang HQ, Zhang YL, Wei G International Journal of Hydrogen Energy, 41(4), 3171, 2016 |
4 |
Mixing augmentation mechanism induced by the pseudo shock wave in transverse gaseous injection flow fields Huang W, Li MH, Yan L International Journal of Hydrogen Energy, 41(25), 10961, 2016 |
5 |
Construction of one-step H-2/O-2 reaction mechanism for predicting ignition and its application in simulation of supersonic combustion Wang B, Wei W, Ma S, Wei G International Journal of Hydrogen Energy, 41(42), 19191, 2016 |
6 |
Study on main flow and fuel injector configurations for Scramjet applications Ali M, Islam AKMS International Journal of Heat and Mass Transfer, 49(19-20), 3634, 2006 |
7 |
Effect of pressure on the extinction, acoustic pressure response, and NO formation in diluted hydrogen-air diffusion flames Sohn CH, Chung SH Combustion and Flame, 121(1-2), 288, 2000 |