QQ客服 官方微博 反馈留言

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 Large Eddy Simulation of Axisymmetric Scramjet Based on Dynamic Zone Flamelet Model 会议论文 Korean Soc Aeronaut & Space Sci, Jeju, SOUTH KOREA, NOV 15-17, 2021 作者:  Sun WM(孙文明);  Liu H(刘航);  Li L(李龙);  Yao W(姚卫) 收藏  |  浏览/下载：16/0  |  提交时间：2022/11/24 Axisymmetric scramjet  Ethylene  Improved Delay Detached Eddy Simulation (IDDES)  Dynamic Zone Flamelet Model (DZFM)  Cavity   Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion 期刊论文 ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350 作者:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军) 收藏  |  浏览/下载：29/0  |  提交时间：2018/12/27 Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions   A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文 Xiamen, China, 6-9 March 2017 作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军) 收藏  |  浏览/下载：35/0  |  提交时间：2018/01/16 Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients