Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-8 of 8 Help

Filters                            
Selected(0)Clear Items/Page:    Sort:
A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  Favorite  |  View/Download：175/49  |  Submit date：2022/07/04
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：338/100  |  Submit date：2019/04/11
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
View  |  Adobe PDF(807Kb)  |  Favorite  |  View/Download：359/114  |  Submit date：2018/07/17
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
View  |  Adobe PDF(805Kb)  |  Favorite  |  View/Download：412/154  |  Submit date：2018/06/06
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(623Kb)  |  Favorite  |  View/Download：272/94  |  Submit date：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(832Kb)  |  Favorite  |  View/Download：296/88  |  Submit date：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  
Characteristics of a supersonic model combustor with two-staged injections of supercritical kerosene 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:  Zhang TC(张泰昌);  Yuan YM(袁越明);  Li JG(李建国);  Fan XJ(范学军);  Zhang TC(张泰昌)
View  |  Adobe PDF(636Kb)  |  Favorite  |  View/Download：561/161  |  Submit date：2014/02/24
Study of turbulent heat transfer of aviation kerosene flows in a curved pipe at supercritical pressure 期刊论文
Applied Thermal Engineering, 2010, 卷号: 30, 期号: 13, 页码: 1845-1851
Authors:  Li XF;  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Huai XL;  Cai J
Adobe PDF(405Kb)  |  Favorite  |  View/Download：1161/311  |  Submit date：2011/03/01