Chinese | English

Scholar Page

Keywords Cloud

Research Outputs

Co-authors[TOP 5]

Usage Statistics


  Total Views
 8822
  Access Source
    internal： 113
    External： 8709
    Domestic： 7912
    Abroad： 910

  Annual Views
 2961
  Access Source
    internal： 11
    External： 2950
    Domestic： 2823
    Abroad： 138

  Monthly Views
 290
  Access Source
    internal： 0
    External： 290
    Domestic： 282
    Abroad： 8

Visits

Visits

1. 热化学非平衡流动中黏性干扰和化学反应对HB2 气动力的影响 [3818]
2. Evolution of cellular structures on oblique detonation surfaces [3526]
3. Instability Criterion of One-Dimensional Detonation Wave with Thre.. [2212]
4. 高焓激波风洞研究进展 [2106]
5. On the numerical technique for the simulation of hypervelocity tes.. [1940]
6. 长试验时间爆轰驱动激波风洞技术研究 [1815]
7. A reconstructed discontinuous Galerkin method based on a Hierarchi.. [1659]
8. Concept of non-ablative thermal protection system for hypersonic v.. [1645]
9. Self-organized generation of transverse waves in diverging cylindr.. [1616]
10. An Integrated Evolutionary Algorithm for Expensive Global Optimiza.. [1573]
11. 高焓激波风洞爆轰驱动技术研究 [1559]
12. 爆轰驱动激波管缝合激波马赫数计算 [1555]
13. 复现飞行条件平板边界层喷流控制实验研究 [1552]
14. 准定常强激波马赫反射波形的数值研究 [1528]
15. 真实比热模型中铝粉尘两相爆轰波的数值研究 [1526]
16. 气体爆轰物理及其统一框架理论 [1519]
17. Cellular Cell Bifurcation Of Cylindrical Detonations [1511]
18. 气相爆轰物理的若干研究进展 [1486]
19. On the transition pattern of the oblique detonation structure [1473]
20. 准定常强激波马赫反射波形结构 [1428]
21. Wave dynamic processes induced by a supersonic projectile discharg.. [1411]
22. 爆轰驱动高焓激波风洞及其瞬态测试技术的研究与进展 [1390]
23. Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels [1346]
24. Approximate analytic solution of heat conduction in hollow semi-sp.. [1337]
25. 高超声速流动上仰异常现象关键因素数值研究 [1301]
26. 用FLUENT软件计算化学氧碘激光流场 [1285]
27. 超声速燃烧室中脉冲爆轰混合/燃烧强化机理研究 [1277]
28. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [1274]
29. Shocked Flows Induced by Supersonic Projectiles Moving in Tubes [1260]
30. 一种激波风洞爆轰双驱动方法和装置 [1251]
31. 环形激波绕射, 反射和聚焦的数值模拟研究 [1231]
32. 基于OH自由基A2Σ + →X2Πr 电子带系发射光谱的温度测量技术 [1228]
33. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [1226]
34. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [1213]
35. 一种具有消波结构的激波风洞真空罐装置 [1197]
36. 三维双楔面定常激波相互作用 [1196]
37. Numerical investigation on the induction zone structure of the obl.. [1196]
38. Numerical simulation of one-dimensional aluminum particle-air deto.. [1193]
39. 建设高温气体动力学国家重点实验室支撑我国高超声速科技发展 [1191]
40. The Structure and Evolution of a Two-Dimensional H2/O2/Ar Cellular.. [1188]
41. Performance of a Detonation Driven Shock Tunnel [1187]
42. Spectral Characteristics of CN Radical (B -> X) and Its Applicatio.. [1186]
43. Numerical and Experimental Investigation of Wave Dynamic Processes.. [1176]
44. 柱面气相散心爆轰波胞格演化规律研究 [1168]
45. Numerical Investigation On The Flowfield Of "Swallowtail" Cavity F.. [1165]
46. 超燃冲压发动机凹腔稳焰器非定常现象的数值研究 [1162]
47. 空心半球高超声速飞行结构传热近似解析求解 [1153]
48. The criterion of the existence or inexistence of transverse shock .. [1148]
49. 爆轰推进概念与机理研究——新型发动机研究的热点 [1145]
50. 爆轰波在楔面上反射数值分析 [1144]
51. Numerical Investigation of Toroidal Shock Wave Focusing in a Cylin.. [1144]
52. 爆轰波在楔面上反射数值分析 [1140]
53. 超高速试验气流的建立与分析 [1135]
54. 高超声速高焓风洞试验技术研究进展 [1134]
55. 脉冲爆轰发动机热射流起爆机理数值分析 [1126]
56. 气相规则胞格爆轰波起爆与传播统一框架的几个关键基础问题研究 [1120]
57. 自由飞试验模型运动参数提取方法 [1120]
58. The cellular structure of a two-dimensional H2/O2/Ar detonation wa.. [1117]
59. 爆轰波在弯管内传播过程数值分析 [1115]
60. 高超声速电离绕流中电子密度的静电探针测量方法研究 [1112]
61. 一种爆轰驱动激波风洞卸爆装置 [1108]
62. 衰减入射激波非定常反射的数值模拟研究 [1102]
63. Analysis of the test condition of a shock-expansion tube: JF-16 [1092]
64. 环形爆轰波在激波管中聚焦的数值模拟 [1083]
65. Abel Inversion of Axially-Symmetric Shock Wave Flows [1079]
66. 一维爆轰波不稳定性的一种理论描述 [1076]
67. 高超声速气动热力学的几个基础研究问题 [1075]
68. 高焓风洞中模型外流场电子密度测试研究 [1075]
69. Experimental Demonstration Of A New Concept Of Drag Reduction And .. [1073]
70. 三维双楔面定常超声速流动研究 [1063]
71. 触摸高温气体动力学 [1061]
72. Analytical and numerical investigations of the reflection of asymm.. [1061]
73. A metamodel-assisted evolutionary algorithm for expensive optimiza.. [1054]
74. 气相爆轰化学反应流场数值模拟 [1053]
75. 高超声速飞行器减阻防热研究进展 [1052]
76. 激波与爆轰波对撞的数值模拟研究 [1049]
77. 正向爆轰驱动高焓激波风洞的数值模拟 [1047]
78. 激波管壁AlO自由基B~2∑~+-X~2∑~+和C~2∏_r-X~2∑~+带系辐射光谱的研.. [1047]
79. 一种基于AUSM思想的通量分裂方法 [1046]
80. Reliable Validation Based on Optical Flow Visualization for CFD Si.. [1044]
81. Numerical investigation on three-dimensional shock wave reflection.. [1041]
82. 气液两相爆轰与气相爆轰绕射的对比与分析 [1037]
83. Heat Transfer Problems Induced By Multi-shocks Interaction [1036]
84. 一维脉冲爆轰波的能量释放规律研究 [1036]
85. Research progress on high-enthalpy and hypersonic flows [1035]
86. Study on the Mechanism of Detonation to Quasi-detonation Transitio.. [1034]
87. 爆轰波穿越惰性气团时的透射激波参数分析 [1032]
88. Three-Dimensional Propagation of the Transmitted Shock Wave in a S.. [1031]
89. 带三维凹槽火焰稳定器的燃烧室放热分布规律研究 [1028]
90. Numerical simulation of deflagration to detonation transition in a.. [1027]
91. 详细化学反应模型中温度修正项特性研究 [1025]
92. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [1022]
93. Numerical analysis of spatial evolution of the small signal gain i.. [1021]
94. 爆轰波与激波对撞爆轰状态演化机理研究 [1021]
95. 激波风洞气动力信号分离的波系适配法 [1012]
96. 超高速高焓流动研究进展 [1003]
97. Dynamic Characteristics of Spherically Converging Detonation Waves [1002]
98. 变截面管道中爆轰胞格演变机制的数值模拟研究 [997]
99. 爆轰驱动高焓激波膨胀管性能研究 [996]
100. 频散可控格式的一种推广形式及其在爆轰波马赫反射中应用 [988]

Downloads

1. 热化学非平衡流动中黏性干扰和化学反应对HB2 气动力的影响 [1743]
2. On the numerical technique for the simulation of hypervelocity tes.. [1054]
3. Evolution of cellular structures on oblique detonation surfaces [958]
4. 真实比热模型中铝粉尘两相爆轰波的数值研究 [835]
5. Instability Criterion of One-Dimensional Detonation Wave with Thre.. [756]
6. Wave dynamic processes induced by a supersonic projectile discharg.. [721]
7. 高超声速高焓风洞试验技术研究进展 [605]
8. A reconstructed discontinuous Galerkin method based on a Hierarchi.. [587]
9. Concept of non-ablative thermal protection system for hypersonic v.. [587]
10. 电子发汗冷却技术及其研究进展 [552]
11. 复现飞行条件平板边界层喷流控制实验研究 [514]
12. 壁面催化效应对高超声速气动热影响研究 [503]
13. Self-organized generation of transverse waves in diverging cylindr.. [494]
14. 高焓流动试验装备与测试技术 [491]
15. 气相爆轰物理的若干研究进展 [490]
16. 准定常强激波马赫反射波形结构 [482]
17. 卷积神经网络在风洞天平静态校准中的应用 [450]
18. 爆轰推进概念与机理研究——新型发动机研究的热点 [447]
19. Performance of a Detonation Driven Shock Tunnel [445]
20. 用FLUENT软件计算化学氧碘激光流场 [441]
21. On the transition pattern of the oblique detonation structure [435]
22. JF-22超高速风洞理论基础与关键技术 [434]
23. An Integrated Evolutionary Algorithm for Expensive Global Optimiza.. [431]
24. Numerical and Experimental Investigation of Wave Dynamic Processes.. [429]
25. 高超声速飞行器减阻防热研究进展 [424]
26. Approximate analytic solution of heat conduction in hollow semi-sp.. [421]
27. The Structure and Evolution of a Two-Dimensional H2/O2/Ar Cellular.. [420]
28. Numerical simulation of one-dimensional aluminum particle-air deto.. [415]
29. 高超声速风洞实验数据多空间相关理论与关联方法研究 [412]
30. Shocked Flows Induced by Supersonic Projectiles Moving in Tubes [409]
31. 准定常强激波马赫反射波形的数值研究 [408]
32. 长试验时间爆轰驱动激波风洞技术研究 [406]
33. Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels [393]
34. 正向爆轰驱动高焓激波风洞的数值模拟 [390]
35. 一维脉冲爆轰波的能量释放规律研究 [390]
36. 三维双楔面定常超声速流动研究 [383]
37. Cellular Cell Bifurcation Of Cylindrical Detonations [381]
38. 单步化学反应模型点火延迟时间研究 [381]
39. 爆轰驱动高焓激波风洞及其瞬态测试技术的研究与进展 [375]
40. 超声速圆柱尾流及其稳定性的数值模拟 [368]
41. 数字图像处理技术在风洞试验中的应用 [364]
42. Numerical investigation of the reflection of unsteady decelerating.. [360]
43. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [356]
44. 一维爆轰波不稳定性的一种理论描述 [356]
45. 频散可控格式的一种推广形式及其在爆轰波马赫反射中应用 [354]
46. The cellular structure of a two-dimensional H2/O2/Ar detonation wa.. [353]
47. 爆轰推进概念与机理研究——新型发动机研究的热点 [352]
48. 环形激波绕射, 反射和聚焦的数值模拟研究 [348]
49. 爆轰驱动激波管缝合激波马赫数计算 [348]
50. 超燃冲压发动机凹腔稳焰器非定常现象的数值研究 [348]
51. Analysis of the test condition of a shock-expansion tube: JF-16 [348]
52. 模拟爆炸波的生物激波管 [347]
53. 风洞实验数据的分析与关联方法 [342]
54. 高超声速电离绕流中电子密度的静电探针测量方法研究 [337]
55. Plasma Assisted Low Temperature Combustion [337]
56. Reconstructing shock front of unstable detonations based on multi-.. [337]
57. 带三维凹槽火焰稳定器的燃烧室放热分布规律研究 [336]
58. 气相规则胞格爆轰波起爆与传播统一框架的几个关键基础问题研究 [332]
59. Numerical investigation on the induction zone structure of the obl.. [332]
60. 气相爆轰高速弹丸速度测量 [328]
61. Micro-shock waves generated inside a fluid jet impinging on plane .. [327]
62. 高焓风洞中模型外流场电子密度测试研究 [327]
63. Heat Transfer Problems Induced By Multi-shocks Interaction [326]
64. Numerical simulation of deflagration to detonation transition in a.. [325]
65. 爆轰波在楔面上反射数值分析 [324]
66. 超高速试验气流的建立与分析 [324]
67. 无缓冲气COIL扩压器流场数值模拟 [323]
68. 脉冲型天平高精度全自动校准系统 [323]
69. 高超声速气动热力学的几个基础研究问题 [321]
70. 基于OH自由基A2Σ + →X2Πr 电子带系发射光谱的温度测量技术 [317]
71. Abel Inversion of Axially-Symmetric Shock Wave Flows [314]
72. Numerical Investigation of Toroidal Shock Wave Focusing in a Cylin.. [314]
73. 分裂算法对准爆轰波数值模拟的影响 [314]
74. 激波风洞气动力信号分离的波系适配法 [313]
75. Aerodynamic measurement of a large aircraft model in hypersonic fl.. [310]
76. Reliable Validation Based on Optical Flow Visualization for CFD Si.. [309]
77. 详细化学反应模型中温度修正项特性研究 [309]
78. 脉冲爆轰发动机热射流起爆机理数值分析 [307]
79. 超高速流动实验设备和相关数值研究 [305]
80. Advances in critical technologies for hypersonic and high-enthalpy.. [305]
81. 空心半球高超声速飞行结构传热近似解析求解 [303]
82. Spectral Characteristics of CN Radical (B -> X) and Its Applicatio.. [300]
83. Comparative study on aerodynamic heating under perfect and nonequi.. [300]
84. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [299]
85. 小尺寸自适应氢氧脉冲爆轰发动机设计和验证 [299]
86. 高焓激波风洞喷管流场数值研究 [299]
87. 气相爆轰化学反应流场数值模拟 [298]
88. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [298]
89. 爆轰驱动高焓激波膨胀管研究 [298]
90. 边界层对驻定斜爆轰结构和稳定性的影响 [298]
91. 自由飞试验模型运动参数提取方法 [297]
92. 先进激波风洞技术研究与进展 [297]
93. Theories and technologies for duplicating hypersonic flight condit.. [297]
94. Effects of different product phases in aluminum dust detonation mo.. [296]
95. Study on the Mechanism of Detonation to Quasi-detonation Transitio.. [295]
96. 柱面气相散心爆轰波胞格演化规律研究 [294]
97. Numerical investigation on three-dimensional shock wave reflection.. [292]
98. 一种激波风洞爆轰双驱动方法和装置 [290]
99. 一种爆轰驱动激波风洞卸爆装置 [288]
100. 超高速高焓流动研究进展 [287]