|
Selected(0)Clear
Items/Page: Sort: |
| Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
Authors: Li B(李波); Yao W(姚卫) ; Fan XJ(范学军)
 Adobe PDF(1358Kb) |  Favorite | View/Download：160/50 | Submit date：2021/02/01 |
| 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：185/64 | Submit date：2020/11/20 |
| Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors: Yao W(姚卫); Wu K(吴坤); Lee YC(李亚超); Fan XJ(范学军)
 Adobe PDF(1156Kb) | Favorite | View/Download：428/0 | Submit date：2018/12/26 |
| 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：273/94 | 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：298/89 | 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 |
| 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
Authors: 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) | Favorite | View/Download：459/95 | Submit date：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
Authors: 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) | Favorite | View/Download：494/179 | Submit date：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 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
Authors: Lu Y(陆阳); Li L(李龙); Fan XJ(范学军)
Adobe PDF(483Kb) | Favorite | View/Download：1008/372 | Submit date：2013/02/28 |
| 轴对称主动冷却发动机燃烧室耦合传热分析方法研究 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors: 陆阳; 袁涛; 李龙; 王晶; 王新竹; 司徒明; 范学军
Adobe PDF(832Kb) | Favorite | View/Download：561/162 | Submit date：2014/01/23
碳氢燃料 主动冷却 耦合传热 数值模拟 |
