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浏览/检索结果: 共12条，第1-10条 帮助 限定条件 发表日期：2017     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 Numerical study of hollow rotating detonation engine with different fuel injection area ratios 期刊论文 PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017 Yao, Songbai; Tang, Xinmeng; Luan, Mingyi; Wang, Jianping 收藏  |  浏览/下载：2/0  |  提交时间：2017/12/03 Rotating detonation engine  Simulation  Hollow combustor  Fuel injection  Propulsion  HYDROGEN-OXYGEN MIXTURE  PROPULSIVE PERFORMANCE  WAVE  COMBUSTOR  MECHANISM  FLOW   Numerical Study of the Propulsive Performance of the Hollow Rotating Detonation Engine with a Laval Nozzle 期刊论文 INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2017 Yao, Songbai; Tang, Xinmeng; Wang, Jianping 收藏  |  浏览/下载：7/0  |  提交时间：2017/12/03 rotating detonation  hollow combustor  Laval nozzle  simulations  HYDROGEN-OXYGEN MIXTURE  MECHANISM  WAVE   A HYBRID APPROACH FOR 3D FULL-FIELD MEASUREMENT ON A CLOSED SLINGER COMBUSTOR BY HYDRAULIC SIMULATIONS 会议论文 Jia, Lichao; Yang, Lili; Yuan, Huijing; Jia, Yongxia; Wang, Yiyang; Feng, Yang 收藏  |  浏览/下载：4/0  |  提交时间：2017/12/03 PARTICLE TRACKING VELOCIMETRY  3-DIMENSIONAL FLOWS  IMAGE VELOCIMETRY   Numerical study of rotating detonation engine with an array of injection holes 期刊论文 SHOCK WAVES, 2017 Yao, S.; Han, X.; Liu, Y.; Wang, J. 收藏  |  浏览/下载：3/0  |  提交时间：2017/12/03 Detonation wave  Rotating detonation engine  Numerical simulation  Injection holes  Transient period  FUEL-AIR MIXTURES  PROPULSIVE PERFORMANCE  HYDROGEN  WAVE  SIMULATION  COMBUSTOR  MECHANISM   Development of zone flamelet model for scramjet combustor modeling 会议论文 Xiamen, China, 6-9 March 2017 作者:  Yao W(姚卫);  Fan XJ(范学军) 收藏  |  浏览/下载：17/0  |  提交时间：2018/01/16 Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft   Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 期刊论文 COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179 作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China. 收藏  |  浏览/下载：15/0  |  提交时间：2017/12/18 Detailed Hydrogen Oxidation Mechanism  Dlr  Flame Stabilization  Sensitivity Analysis  Supersonic Combustion   LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文 Xiamen, China, 6-9 March 2017 作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk) 收藏  |  浏览/下载：19/0  |  提交时间：2018/01/16 Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow   Development of zone flamelet modelfor scramjet combustor modeling 会议论文 Xiamen, China, March 6, 2017 - March 9, 2017 作者:  Yao W(姚卫);  Fan XJ(范学军) 收藏  |  浏览/下载：30/0  |  提交时间：2018/11/08 Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion   Near limit premixed flamelets in Hele-Shaw cells 期刊论文 PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 1, 页码: 1585-1593 作者:  Chen XT;  Lu ZB;  Wang SF(王双峰) 收藏  |  浏览/下载：24/0  |  提交时间：2017/07/24 Premixed flame  Flame cylinder  Hele-Shaw cell  Near limit  Narrow channel   ANALYTICAL STUDY OF LOW-FREQUENCY HELMHOLTZ MODE OSCILLATION IN A MODEL COMBUSTOR 会议论文 ASME Turbo Expo: Turbine Technical Conference and Exposition, Charlotte, NC, 2017-06-26 作者:  Zhang, Man;  Lin, Yuzhen;  Tao, Wenjie 收藏  |  浏览/下载：5/0  |  提交时间：2019/12/30 combustion instability  Helmholtz  harmonic wave  low-order modeling