中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共5条，第1-5条 帮助

限定条件            
已选(0)清除 条数/页：   排序方式：
Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
作者:  Yao W(姚卫);  Chen L(陈留)
Adobe PDF(2272Kb)  |  收藏  |  浏览/下载：262/145  |  提交时间：2021/06/11
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor 会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
作者:  Cheng D(程迪);  Wang J(王晶);  Gong J;  Lu Y(陆阳);  Yao W(姚卫);  Li L(李龙);  Fan XJ(范学军);  Fan, Xuejun (xfan@imech.ac.cn)
浏览  |  Adobe PDF(2131Kb)  |  收藏  |  浏览/下载：322/123  |  提交时间：2017/05/05
Equivalence Ratios  Heat Flux Distributions  Heat Transfer Characteristics  Scramjet  Supercritical Kerosenes  Supersonic Combustion  Supersonic Combustors  Total Temperatures  
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
作者:  Lu Y(陆阳);  Wang XZ(王新竹);  Li L(李龙);  Cheng D(程迪);  Yuan T(袁涛);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(445Kb)  |  收藏  |  浏览/下载：426/91  |  提交时间：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
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)
Adobe PDF(1195Kb)  |  收藏  |  浏览/下载：474/173  |  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  
A comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Li XP(李晓鹏);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(728Kb)  |  收藏  |  浏览/下载：274/88  |  提交时间：2017/05/05
Comparative Studies  Flow Charac  Teristics  High Order Harmonics  High Resolution  Instability Modes  Near  Field Structure  Shock Structure  Under  Expanded Jets