IMECH-IR
(Note: the search results are based on claimed items)

Browse/Search Results:  1-10 of 10 Help

Filters                            
Selected(0)Clear Items/Page:    Sort:
主动冷却超燃冲压发动机的起动方法和起动装置 专利
发明专利. 主动冷却超燃冲压发动机的起动方法和起动装置, 专利号: ZL201810159005.7, 申请日期: 2018-02-26,
Inventors:  张泰昌;  袁涛;  范学军
View  |  Adobe PDF(513Kb)  |  Favorite  |  View/Download:475/51  |  Submit date:2020/02/10
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
Authors:  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)
View  |  Adobe PDF(2651Kb)  |  Favorite  |  View/Download:414/135  |  Submit date:2019/09/09
Heat flux measurement  Kerosene  Supersonic combustion  Scramjet  Heat flux sensor  
Hypergolic ignition modulated by head-on collision, intermixing and convective cooling of binary droplets with varying sizes 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 139, 页码: 475-481
Authors:  Zhang DW;  Yu DH;  Zhang P;  Yuan YM(袁越明);  Yue LJ(岳连捷);  Zhang TC(张泰昌);  Fan XJ(范学军)
View  |  Adobe PDF(1528Kb)  |  Favorite  |  View/Download:326/120  |  Submit date:2019/09/09
一种用于超声速然烧的直连台的气膜冷却装置 专利
发明专利. 一种用于超声速然烧的直连台的气膜冷却装置, 专利号: ZL201611135726.1, 申请日期: 2016-12-12,
Inventors:  樊川;  王晶;  孟令瑾;  范学军
View  |  Adobe PDF(336Kb)  |  Favorite  |  View/Download:244/50  |  Submit date:2020/02/09
不同喷压比下欠膨胀射流对特征频率激励的响应 期刊论文
推进技术, 2019, 卷号: 40, 期号: 06, 页码: 1239-1246
Authors:  李晓鹏;  周蕊;  庄法坤;  曹逻炜;  谢国山;  范学军
View  |  Adobe PDF(6645Kb)  |  Favorite  |  View/Download:381/51  |  Submit date:2019/09/12
欠膨胀射流  喷压比  特征频率激励  大涡模拟  流动响应  
Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
Authors:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(862Kb)  |  Favorite  |  View/Download:334/100  |  Submit date:2019/04/11
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1820Kb)  |  Favorite  |  View/Download:471/159  |  Submit date:2018/12/27
Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio  
Influence of compressibility effect on supersonic combustion modeling 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Chen L;  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1280Kb)  |  Favorite  |  View/Download:172/72  |  Submit date:2020/11/20
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
Authors:  Li X(李轩);  Lu Y(陆阳);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(705Kb)  |  Favorite  |  View/Download:183/63  |  Submit date:2020/11/20
Modeling Analysis on Cavity-based Flame Stabilization in Scramjet Combustor 会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Fan XJ(范学军)
Favorite  |  View/Download:141/0  |  Submit date:2019/11/20
Combustion chemistry  Combustion dynamics  Dual  mode scramjet  Flame stabilization  Improved delayed detached eddy simulations  Overall reactions  Scramjet combustors  Shock  wave structures