1001-4055
2013 Issue 12
A Combined CFD/Characteristic Method for Design and Performance Prediciton of Hypersonic Inlet with Leading Edge Bluntness
gao wen zhi ;, li zhu fei ;, tan hui jun ;, yang ji ming ;
gao wen zhi ;, li zhu fei ;, tan hui jun ;, yang ji ming ;
..............page:1585-1592
Experimental Investigation of Constant Pressure Gradient Curved Compression System in Non-Uniform Inflow
jin feng ;, pan zuo ;, zhang yuan ;
jin feng ;, pan zuo ;, zhang yuan ;
..............page:1593-1600
Reverse Design and Optimization of 2D Hypersonic Curved Shock Compression Inlet Based on Given Wall Pressure Distribution
jin zhi guang ;, li yong zhou ;, wang lei ;, zhang yuan ;, zhang lin ;
jin zhi guang ;, li yong zhou ;, wang lei ;, zhang yuan ;, zhang lin ;
..............page:1601-1605
Research on Mass-Flow Controlling Technology of TBCC Axisymmetric Inlet
guo rong wei ;, wang ya gang ;, yuan hua cheng ;
guo rong wei ;, wang ya gang ;, yuan hua cheng ;
..............page:1606-1615
Properties of Capture Stream Tube Contraction Ratio and Application of 2D Supersonic Inlet
guan xiang dong ;, li hong dong ;, meng yu peng ;, zhu shou mei ;
guan xiang dong ;, li hong dong ;, meng yu peng ;, zhu shou mei ;
..............page:1616-1620
Analysis for Thermal and Mechanical Coupling in Active Cooling Channels for Engine Combustor
bai zuo guang ;, gao xiao wei ;, yuan zhi chao ;, zhang yu guang ;
bai zuo guang ;, gao xiao wei ;, yuan zhi chao ;, zhang yu guang ;
..............page:1621-1627
Experimental Research on Ethylene Ignition with Hydrogen Self-Ignition Assistant at Mach 4
cheng wen ming ;, deng wei zuo ;, le jia ling ;, yang shun hua ;, zhang wan zhou ;
cheng wen ming ;, deng wei zuo ;, le jia ling ;, yang shun hua ;, zhang wan zhou ;
..............page:1628-1635
Effects of Different Fueled Combustion Heater on Scramjet Performance
li wei qiang ;, xiao bao guo ;, xing jian wen ;
li wei qiang ;, xiao bao guo ;, xing jian wen ;
..............page:1636-1642
Numerical Simulations on RBCC Engine in Scramjet/Rocket Mode
he guo qiang ;, qin fei ;, tang xiang ;
he guo qiang ;, qin fei ;, tang xiang ;
..............page:1643-1649
Numerical Simulation of Supersonic Turbulent Combustion Flows Based on Flamelet Model
chen bing ;, xu xu ;, zhang yan ;
chen bing ;, xu xu ;, zhang yan ;
..............page:1650-1658
Design and Consideration of Active and Passive Combined Thermal Protection System of Scramjet
bao wen ;, qin jiang ;, yu da ren ;, zhang cong ;
bao wen ;, qin jiang ;, yu da ren ;, zhang cong ;
..............page:1659-1663
Theoretical Study for Heat Transfer of Ramjet Fuel Tank
han jiang feng ;, li li han ;, zhang xiao ge ;, zheng ri heng ;
han jiang feng ;, li li han ;, zhang xiao ge ;, zheng ri heng ;
..............page:1664-1669
Research of Ablative Material Reconstruction and Its Internal Flow and Heat Transfer
chen hong ;, han ding ;, zhang hui jie ;, zhu wei bing ;
chen hong ;, han ding ;, zhang hui jie ;, zhu wei bing ;
..............page:1670-1676
Combustion Performance Study of Side Dump Heater
chen jing min ;, li li han ;, li zhi yong ;, wang deng yun ;, wang hong mei ;
chen jing min ;, li li han ;, li zhi yong ;, wang deng yun ;, wang hong mei ;
..............page:1677-1681
Investigation on Deposit Property of C/SiC Composite Nozzle for Ramjet
chen jing min ;, li li han ;, li zhi yong ;, zheng ri heng ;
chen jing min ;, li li han ;, li zhi yong ;, zheng ri heng ;
..............page:1682-1689
Study on Multi-Variable Control System for Variable Geometry Liquid Ramjet Engine
liu han bin ;, nie zuo cong ;, pu sheng zhi ;, wu zhi feng ;
liu han bin ;, nie zuo cong ;, pu sheng zhi ;, wu zhi feng ;
..............page:1690-1695
Research on Application of Variable Universe Fuzzy Control in Mach Number Control for UVA
li lin yu ;, liu han bin ;, ren feng sheng ;, zhang zhen jia ;, zhang zheng wei ;
li lin yu ;, liu han bin ;, ren feng sheng ;, zhang zhen jia ;, zhang zheng wei ;
..............page:1696-1701
Effects of Fuel Cracking Characteristic on Stability of Fuel Supply System
bao wen ;, ge xu mei ;, yu bin ;, yu da ren ;, yu wen li ;, zhou wei xing ;
bao wen ;, ge xu mei ;, yu bin ;, yu da ren ;, yu wen li ;, zhou wei xing ;
..............page:1702-1707
Evaluation of Fuel Vapor Turbine Capacity for Doing Work Onboard for a Hydrocarbon Fueled Scramjet
bao wen ;, li lin lin ;, qin jiang ;, zhang zuo ;
bao wen ;, li lin lin ;, qin jiang ;, zhang zuo ;
..............page:1708-1712
Inhibition Mechanism of Pyrolytic Cokes from Endothermic Hydrocarbon Fuels in Regenerative Cooling Channels
hu shen lin ;, liu guo zhu ;, ma xue song ;, wang xu qing ;, zhang qiang qiang ;, zhang xiang wen ;
hu shen lin ;, liu guo zhu ;, ma xue song ;, wang xu qing ;, zhang qiang qiang ;, zhang xiang wen ;
..............page:1713-1718
An Overview on Mode Transition in Dual Mode Ramjet
li xuan ;, liu gang ;, xu xu ;, zhang yan ;, zhu shao hua ;
li xuan ;, liu gang ;, xu xu ;, zhang yan ;, zhu shao hua ;
..............page:1719-1728