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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 [3816]
2. Evolution of cellular structures on oblique detonation surfaces [3531]
3. Instability Criterion of One-Dimensional Detonation Wave with Thre.. [2217]
4. 高焓激波风洞研究进展 [2110]
5. On the numerical technique for the simulation of hypervelocity tes.. [1942]
6. 长试验时间爆轰驱动激波风洞技术研究 [1820]
7. A reconstructed discontinuous Galerkin method based on a Hierarchi.. [1676]
8. Concept of non-ablative thermal protection system for hypersonic v.. [1673]
9. Self-organized generation of transverse waves in diverging cylindr.. [1624]
10. An Integrated Evolutionary Algorithm for Expensive Global Optimiza.. [1580]
11. 高焓激波风洞爆轰驱动技术研究 [1570]
12. 爆轰驱动激波管缝合激波马赫数计算 [1559]
13. 复现飞行条件平板边界层喷流控制实验研究 [1558]
14. 准定常强激波马赫反射波形的数值研究 [1534]
15. 真实比热模型中铝粉尘两相爆轰波的数值研究 [1530]
16. 气体爆轰物理及其统一框架理论 [1521]
17. Cellular Cell Bifurcation Of Cylindrical Detonations [1513]
18. 气相爆轰物理的若干研究进展 [1493]
19. On the transition pattern of the oblique detonation structure [1487]
20. 准定常强激波马赫反射波形结构 [1433]
21. Wave dynamic processes induced by a supersonic projectile discharg.. [1420]
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 [1393]
23. Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels [1355]
24. Approximate analytic solution of heat conduction in hollow semi-sp.. [1345]
25. 高超声速流动上仰异常现象关键因素数值研究 [1306]
26. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [1278]
27. 超声速燃烧室中脉冲爆轰混合/燃烧强化机理研究 [1278]
28. 用FLUENT软件计算化学氧碘激光流场 [1275]
29. Shocked Flows Induced by Supersonic Projectiles Moving in Tubes [1266]
30. 一种激波风洞爆轰双驱动方法和装置 [1254]
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 [1231]
33. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [1227]
34. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [1223]
35. Numerical investigation on the induction zone structure of the obl.. [1211]
36. Numerical and Experimental Investigation of Wave Dynamic Processes.. [1207]
37. Numerical simulation of one-dimensional aluminum particle-air deto.. [1203]
38. 三维双楔面定常激波相互作用 [1202]
39. 一种具有消波结构的激波风洞真空罐装置 [1200]
40. The Structure and Evolution of a Two-Dimensional H2/O2/Ar Cellular.. [1197]
41. Spectral Characteristics of CN Radical (B -> X) and Its Applicatio.. [1195]
42. 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 [1194]
43. Performance of a Detonation Driven Shock Tunnel [1190]
44. 柱面气相散心爆轰波胞格演化规律研究 [1173]
45. Numerical Investigation On The Flowfield Of "Swallowtail" Cavity F.. [1170]
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 [1159]
48. The criterion of the existence or inexistence of transverse shock .. [1157]
49. 爆轰推进概念与机理研究——新型发动机研究的热点 [1153]
50. 爆轰波在楔面上反射数值分析 [1149]
51. Numerical Investigation of Toroidal Shock Wave Focusing in a Cylin.. [1147]
52. 爆轰波在楔面上反射数值分析 [1144]
53. 超高速试验气流的建立与分析 [1139]
54. 自由飞试验模型运动参数提取方法 [1135]
55. 高超声速高焓风洞试验技术研究进展 [1135]
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 [1131]
57. 脉冲爆轰发动机热射流起爆机理数值分析 [1128]
58. The cellular structure of a two-dimensional H2/O2/Ar detonation wa.. [1127]
59. 爆轰波在弯管内传播过程数值分析 [1118]
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 [1115]
61. 一种爆轰驱动激波风洞卸爆装置 [1113]
62. 衰减入射激波非定常反射的数值模拟研究 [1105]
63. Analysis of the test condition of a shock-expansion tube: JF-16 [1098]
64. 环形爆轰波在激波管中聚焦的数值模拟 [1088]
65. Abel Inversion of Axially-Symmetric Shock Wave Flows [1086]
66. Experimental Demonstration Of A New Concept Of Drag Reduction And .. [1083]
67. 高超声速气动热力学的几个基础研究问题 [1082]
68. 一维爆轰波不稳定性的一种理论描述 [1075]
69. 高焓风洞中模型外流场电子密度测试研究 [1071]
70. 触摸高温气体动力学 [1070]
71. Analytical and numerical investigations of the reflection of asymm.. [1069]
72. 气相爆轰化学反应流场数值模拟 [1064]
73. 高超声速飞行器减阻防热研究进展 [1060]
74. 三维双楔面定常超声速流动研究 [1057]
75. A metamodel-assisted evolutionary algorithm for expensive optimiza.. [1055]
76. 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.. [1054]
77. 激波与爆轰波对撞的数值模拟研究 [1053]
78. 正向爆轰驱动高焓激波风洞的数值模拟 [1052]
79. 一种基于AUSM思想的通量分裂方法 [1049]
80. Reliable Validation Based on Optical Flow Visualization for CFD Si.. [1048]
81. Numerical investigation on three-dimensional shock wave reflection.. [1046]
82. Heat Transfer Problems Induced By Multi-shocks Interaction [1043]
83. Study on the Mechanism of Detonation to Quasi-detonation Transitio.. [1039]
84. Research progress on high-enthalpy and hypersonic flows [1038]
85. Numerical simulation of deflagration to detonation transition in a.. [1038]
86. 气液两相爆轰与气相爆轰绕射的对比与分析 [1037]
87. Three-Dimensional Propagation of the Transmitted Shock Wave in a S.. [1034]
88. 详细化学反应模型中温度修正项特性研究 [1034]
89. 爆轰波穿越惰性气团时的透射激波参数分析 [1033]
90. 带三维凹槽火焰稳定器的燃烧室放热分布规律研究 [1032]
91. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [1031]
92. Numerical analysis of spatial evolution of the small signal gain i.. [1031]
93. 一维脉冲爆轰波的能量释放规律研究 [1031]
94. 爆轰波与激波对撞爆轰状态演化机理研究 [1025]
95. 激波风洞气动力信号分离的波系适配法 [1016]
96. Dynamic Characteristics of Spherically Converging Detonation Waves [1009]
97. 超高速高焓流动研究进展 [1007]
98. 爆轰驱动高焓激波膨胀管性能研究 [1002]
99. 变截面管道中爆轰胞格演变机制的数值模拟研究 [1001]
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 [990]

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 [1740]
2. On the numerical technique for the simulation of hypervelocity tes.. [1054]
3. Evolution of cellular structures on oblique detonation surfaces [962]
4. 真实比热模型中铝粉尘两相爆轰波的数值研究 [838]
5. Instability Criterion of One-Dimensional Detonation Wave with Thre.. [760]
6. Wave dynamic processes induced by a supersonic projectile discharg.. [729]
7. Concept of non-ablative thermal protection system for hypersonic v.. [614]
8. 高超声速高焓风洞试验技术研究进展 [605]
9. A reconstructed discontinuous Galerkin method based on a Hierarchi.. [603]
10. 电子发汗冷却技术及其研究进展 [565]
11. 复现飞行条件平板边界层喷流控制实验研究 [518]
12. 壁面催化效应对高超声速气动热影响研究 [505]
13. Self-organized generation of transverse waves in diverging cylindr.. [501]
14. 高焓流动试验装备与测试技术 [498]
15. 气相爆轰物理的若干研究进展 [496]
16. 准定常强激波马赫反射波形结构 [485]
17. Numerical and Experimental Investigation of Wave Dynamic Processes.. [459]
18. 爆轰推进概念与机理研究——新型发动机研究的热点 [454]
19. JF-22超高速风洞理论基础与关键技术 [453]
20. 卷积神经网络在风洞天平静态校准中的应用 [449]
21. On the transition pattern of the oblique detonation structure [448]
22. Performance of a Detonation Driven Shock Tunnel [447]
23. An Integrated Evolutionary Algorithm for Expensive Global Optimiza.. [437]
24. 高超声速飞行器减阻防热研究进展 [431]
25. 用FLUENT软件计算化学氧碘激光流场 [430]
26. The Structure and Evolution of a Two-Dimensional H2/O2/Ar Cellular.. [428]
27. Approximate analytic solution of heat conduction in hollow semi-sp.. [428]
28. Numerical simulation of one-dimensional aluminum particle-air deto.. [424]
29. Shocked Flows Induced by Supersonic Projectiles Moving in Tubes [414]
30. 准定常强激波马赫反射波形的数值研究 [413]
31. 长试验时间爆轰驱动激波风洞技术研究 [410]
32. Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels [401]
33. 高超声速风洞实验数据多空间相关理论与关联方法研究 [401]
34. 正向爆轰驱动高焓激波风洞的数值模拟 [394]
35. 一维脉冲爆轰波的能量释放规律研究 [384]
36. Cellular Cell Bifurcation Of Cylindrical Detonations [382]
37. 爆轰驱动高焓激波风洞及其瞬态测试技术的研究与进展 [377]
38. 单步化学反应模型点火延迟时间研究 [377]
39. 三维双楔面定常超声速流动研究 [376]
40. 数字图像处理技术在风洞试验中的应用 [372]
41. 超声速圆柱尾流及其稳定性的数值模拟 [369]
42. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [365]
43. Numerical investigation of the reflection of unsteady decelerating.. [364]
44. The cellular structure of a two-dimensional H2/O2/Ar detonation wa.. [362]
45. 爆轰推进概念与机理研究——新型发动机研究的热点 [360]
46. 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 [355]
47. 一维爆轰波不稳定性的一种理论描述 [354]
48. Analysis of the test condition of a shock-expansion tube: JF-16 [353]
49. 爆轰驱动激波管缝合激波马赫数计算 [351]
50. 模拟爆炸波的生物激波管 [349]
51. Plasma Assisted Low Temperature Combustion [348]
52. 环形激波绕射, 反射和聚焦的数值模拟研究 [347]
53. 超燃冲压发动机凹腔稳焰器非定常现象的数值研究 [346]
54. Numerical investigation on the induction zone structure of the obl.. [346]
55. 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 [342]
56. 风洞实验数据的分析与关联方法 [342]
57. 带三维凹槽火焰稳定器的燃烧室放热分布规律研究 [339]
58. 高超声速电离绕流中电子密度的静电探针测量方法研究 [339]
59. Numerical simulation of deflagration to detonation transition in a.. [335]
60. Reconstructing shock front of unstable detonations based on multi-.. [335]
61. Micro-shock waves generated inside a fluid jet impinging on plane .. [332]
62. Heat Transfer Problems Induced By Multi-shocks Interaction [332]
63. 气相爆轰高速弹丸速度测量 [330]
64. 爆轰波在楔面上反射数值分析 [327]
65. 高超声速气动热力学的几个基础研究问题 [327]
66. 超高速试验气流的建立与分析 [327]
67. 脉冲型天平高精度全自动校准系统 [326]
68. 高焓风洞中模型外流场电子密度测试研究 [322]
69. Abel Inversion of Axially-Symmetric Shock Wave Flows [320]
70. 分裂算法对准爆轰波数值模拟的影响 [320]
71. 基于OH自由基A2Σ + →X2Πr 电子带系发射光谱的温度测量技术 [319]
72. 详细化学反应模型中温度修正项特性研究 [317]
73. Numerical Investigation of Toroidal Shock Wave Focusing in a Cylin.. [316]
74. 激波风洞气动力信号分离的波系适配法 [316]
75. 无缓冲气COIL扩压器流场数值模拟 [314]
76. Comparative study on aerodynamic heating under perfect and nonequi.. [313]
77. Reliable Validation Based on Optical Flow Visualization for CFD Si.. [312]
78. 自由飞试验模型运动参数提取方法 [311]
79. 超高速流动实验设备和相关数值研究 [309]
80. 气相爆轰化学反应流场数值模拟 [308]
81. 脉冲爆轰发动机热射流起爆机理数值分析 [308]
82. Spectral Characteristics of CN Radical (B -> X) and Its Applicatio.. [308]
83. 空心半球高超声速飞行结构传热近似解析求解 [308]
84. 高焓激波风洞喷管流场数值研究 [307]
85. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [306]
86. Advances in critical technologies for hypersonic and high-enthalpy.. [305]
87. Aerodynamic measurement of a large aircraft model in hypersonic fl.. [304]
88. 小尺寸自适应氢氧脉冲爆轰发动机设计和验证 [303]
89. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [302]
90. Effects of different product phases in aluminum dust detonation mo.. [302]
91. 先进激波风洞技术研究与进展 [300]
92. Study on the Mechanism of Detonation to Quasi-detonation Transitio.. [299]
93. 边界层对驻定斜爆轰结构和稳定性的影响 [299]
94. 柱面气相散心爆轰波胞格演化规律研究 [298]
95. Numerical investigation on three-dimensional shock wave reflection.. [296]
96. 爆轰驱动高焓激波膨胀管研究 [292]
97. 一种激波风洞爆轰双驱动方法和装置 [292]
98. 一种爆轰驱动激波风洞卸爆装置 [291]
99. 超高速高焓流动研究进展 [290]
100. Theories and technologies for duplicating hypersonic flight condit.. [290]