IMECH-IR

浏览/检索结果: 共9条,第1-9条 帮助

限定条件            
已选(0)清除 条数/页:   排序方式:
Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
作者:  Cheng D(程迪);  Wang J(王晶);  Lu Y(陆阳);  Li L(李龙);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(2651Kb)  |  收藏  |  浏览/下载:409/133  |  提交时间:2019/09/09
Heat flux measurement  Kerosene  Supersonic combustion  Scramjet  Heat flux sensor  
A novel method of cooling channel optimization for active-cooled structure using the calculus of variations 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:  Li X(李轩);  Lu Y(陆阳);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(705Kb)  |  收藏  |  浏览/下载:180/62  |  提交时间:2020/11/20
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Li B;  Lee YC(李亚超);  Yao W(姚卫);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1813Kb)  |  收藏  |  浏览/下载:313/84  |  提交时间:2018/12/26
Development of a radiative heating facility for studying flow and heat transfer in hydrocarbon-cooled structures 期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2018, 卷号: 89, 期号: 6, 页码: 64901
作者:  Dong D(董达);  Lu Y(陆阳);  Yuan YM(袁越明);  Fan XJ(范学军)
浏览  |  Adobe PDF(4017Kb)  |  收藏  |  浏览/下载:477/101  |  提交时间:2018/10/30
Development of a radiative heating system for studies of heat transfer in fuel-cooled structures 会议论文
14th International Energy Conversion Engineering Conference, Salt Lake City, UT, JUL 25-27, 2016
作者:  Dong D(董达);  Lu Y(陆阳);  Yuan YM(袁越明);  Fan XJ(范学军);  Dong, D (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(637Kb)  |  收藏  |  浏览/下载:298/75  |  提交时间:2017/05/12
Aviation Kerosene  Supercritical Conditions  Pressure  Rp-3  
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:329/125  |  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:440/92  |  提交时间:2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
主动冷却燃烧室燃烧与传热耦合过程迭代分析设计方法 期刊论文
推进技术, 2014, 卷号: 35, 期号: 2, 页码: 213-219
作者:  王新竹;  张泰昌;  陆阳;  范学军
Adobe PDF(795Kb)  |  收藏  |  浏览/下载:706/144  |  提交时间:2014/11/05
超燃冲压发动机  主动冷却  碳氢燃料  耦合传热  闭环运行  
A Thermal Analysis Method for Fuel-Cooled Combustor Structure based on Heat Flux Measurement 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference., Tours,France, 2012.9.24-28
作者:  Lu Y(陆阳);  Li L(李龙);  Fan XJ(范学军)
浏览  |  Adobe PDF(483Kb)  |  收藏  |  浏览/下载:1001/369  |  提交时间:2013/02/28