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浏览/检索结果: 共3条，第1-3条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015 作者:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军) 收藏  |  浏览/下载：16/0  |  提交时间：2016/07/01 Adiabatic flame temperature  Combustion  Directed graphs  Flow separation  Heat flux  Kerosene  Large eddy simulation  Musculoskeletal system  Real time systems  Sensitivity analysis  Spacecraft  Transients   The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor 期刊论文 JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 371,380 Mohammad Ali; S. Ahmed; A.K.M. Sadrul Islam 收藏  |  浏览/下载：11/0  |  提交时间：2013/03/12 scramjet engine  TVD scheme  finite width of inlet  supersonic mixing  parallel air stream  flame holding.   The Effect of Injection Angle on Mixing and Flame Holding in Supersonic Combustor 期刊论文 JOURNAL OF THERMAL SCIENCE, 2002, 卷号: 11, 期号: 1, 页码: 80,91 Shakil Ahmed; Mohammad Ali; A. K. M. Sadrul Islam 收藏  |  浏览/下载：8/0  |  提交时间：2013/03/12 scramjet engine  TVD scheme  backward-facing step  supersonic mixing  supersonic stream  flame holding.