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| 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：189/51 | Submit date：2022/07/04 |
| 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
Authors: Yao W(姚卫); Chen L(陈留)
Adobe PDF(2272Kb) | Favorite | View/Download：297/153 | Submit date：2021/06/11 |
| Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors: Jiang ZL(姜宗林); Yu HR(俞鸿儒)
 View | Adobe PDF(523Kb) | Favorite | View/Download：545/75 | Submit date：2020/01/06 |
| Aerodynamic Force Measurement Techniques in JF12 Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors: Liu YF(刘云峰); Wang YP(汪运鹏); Yuan CK(苑朝凯); Luo ZT(罗长童); Jiang ZL(姜宗林)
View | Adobe PDF(532Kb) | Favorite | View/Download：214/78 | Submit date：2020/01/06 |
| 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：428/163 | Submit date：2018/06/06 |
| AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林); Teng HH(滕宏辉)
View | Adobe PDF(4139Kb) | Favorite | View/Download：314/70 | Submit date：2019/04/19 |
| 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：298/105 | 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：315/95 | 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 |
| 高超声速下三维侧压进气道激波干扰的研究 会议论文
中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议, 中国陕西西安, 2016-08-17
Authors: 项高翔; 王春; 姜宗林
View | Adobe PDF(892Kb) | Favorite | View/Download：310/74 | Submit date：2017/09/27
高超声速流动 体-翼激波干扰 波系结构 流场区域 |
| Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
Authors: Gan JY; Shen YQ(申义庆); Zha GC
View | Adobe PDF(555Kb) | Favorite | View/Download：313/100 | Submit date：2017/05/05
Central Differencing Drag Prediction Finite Difference Scheme High Order Scheme Line Relaxation Mesh Refinement Trailing Edges Turbulent Models |
