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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 [3812]
2. Evolution of cellular structures on oblique detonation surfaces [3530]
3. Instability Criterion of One-Dimensional Detonation Wave with Thre.. [2214]
4. 高焓激波风洞研究进展 [2110]
5. On the numerical technique for the simulation of hypervelocity tes.. [1935]
6. 长试验时间爆轰驱动激波风洞技术研究 [1818]
7. A reconstructed discontinuous Galerkin method based on a Hierarchi.. [1662]
8. Concept of non-ablative thermal protection system for hypersonic v.. [1653]
9. Self-organized generation of transverse waves in diverging cylindr.. [1618]
10. An Integrated Evolutionary Algorithm for Expensive Global Optimiza.. [1574]
11. 高焓激波风洞爆轰驱动技术研究 [1561]
12. 爆轰驱动激波管缝合激波马赫数计算 [1557]
13. 复现飞行条件平板边界层喷流控制实验研究 [1557]
14. 准定常强激波马赫反射波形的数值研究 [1530]
15. 真实比热模型中铝粉尘两相爆轰波的数值研究 [1527]
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 [1492]
19. On the transition pattern of the oblique detonation structure [1475]
20. 准定常强激波马赫反射波形结构 [1431]
21. Wave dynamic processes induced by a supersonic projectile discharg.. [1416]
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 [1347]
24. Approximate analytic solution of heat conduction in hollow semi-sp.. [1342]
25. 高超声速流动上仰异常现象关键因素数值研究 [1303]
26. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [1277]
27. 超声速燃烧室中脉冲爆轰混合/燃烧强化机理研究 [1277]
28. 用FLUENT软件计算化学氧碘激光流场 [1274]
29. Shocked Flows Induced by Supersonic Projectiles Moving in Tubes [1261]
30. 一种激波风洞爆轰双驱动方法和装置 [1253]
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 [1229]
33. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [1227]
34. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [1217]
35. 一种具有消波结构的激波风洞真空罐装置 [1199]
36. Numerical investigation on the induction zone structure of the obl.. [1199]
37. 三维双楔面定常激波相互作用 [1198]
38. Numerical simulation of one-dimensional aluminum particle-air deto.. [1197]
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 [1193]
40. The Structure and Evolution of a Two-Dimensional H2/O2/Ar Cellular.. [1189]
41. Performance of a Detonation Driven Shock Tunnel [1188]
42. Spectral Characteristics of CN Radical (B -> X) and Its Applicatio.. [1186]
43. Numerical and Experimental Investigation of Wave Dynamic Processes.. [1179]
44. 柱面气相散心爆轰波胞格演化规律研究 [1172]
45. Numerical Investigation On The Flowfield Of "Swallowtail" Cavity F.. [1168]
46. 超燃冲压发动机凹腔稳焰器非定常现象的数值研究 [1159]
47. 空心半球高超声速飞行结构传热近似解析求解 [1155]
48. The criterion of the existence or inexistence of transverse shock .. [1153]
49. 爆轰推进概念与机理研究——新型发动机研究的热点 [1149]
50. 爆轰波在楔面上反射数值分析 [1146]
51. Numerical Investigation of Toroidal Shock Wave Focusing in a Cylin.. [1146]
52. 爆轰波在楔面上反射数值分析 [1142]
53. 超高速试验气流的建立与分析 [1137]
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 [1127]
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 [1126]
57. 自由飞试验模型运动参数提取方法 [1121]
58. The cellular structure of a two-dimensional H2/O2/Ar detonation wa.. [1120]
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 [1113]
61. 一种爆轰驱动激波风洞卸爆装置 [1111]
62. 衰减入射激波非定常反射的数值模拟研究 [1104]
63. Analysis of the test condition of a shock-expansion tube: JF-16 [1094]
64. 环形爆轰波在激波管中聚焦的数值模拟 [1085]
65. Abel Inversion of Axially-Symmetric Shock Wave Flows [1082]
66. 高超声速气动热力学的几个基础研究问题 [1079]
67. Experimental Demonstration Of A New Concept Of Drag Reduction And .. [1077]
68. 一维爆轰波不稳定性的一种理论描述 [1073]
69. 高焓风洞中模型外流场电子密度测试研究 [1068]
70. Analytical and numerical investigations of the reflection of asymm.. [1066]
71. 触摸高温气体动力学 [1064]
72. 气相爆轰化学反应流场数值模拟 [1058]
73. A metamodel-assisted evolutionary algorithm for expensive optimiza.. [1055]
74. 高超声速飞行器减阻防热研究进展 [1054]
75. 激波与爆轰波对撞的数值模拟研究 [1052]
76. 三维双楔面定常超声速流动研究 [1051]
77. 正向爆轰驱动高焓激波风洞的数值模拟 [1050]
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.. [1049]
79. 一种基于AUSM思想的通量分裂方法 [1047]
80. Reliable Validation Based on Optical Flow Visualization for CFD Si.. [1046]
81. Numerical investigation on three-dimensional shock wave reflection.. [1044]
82. Heat Transfer Problems Induced By Multi-shocks Interaction [1040]
83. 气液两相爆轰与气相爆轰绕射的对比与分析 [1036]
84. Study on the Mechanism of Detonation to Quasi-detonation Transitio.. [1035]
85. Research progress on high-enthalpy and hypersonic flows [1034]
86. Three-Dimensional Propagation of the Transmitted Shock Wave in a S.. [1033]
87. 爆轰波穿越惰性气团时的透射激波参数分析 [1033]
88. Numerical simulation of deflagration to detonation transition in a.. [1031]
89. 带三维凹槽火焰稳定器的燃烧室放热分布规律研究 [1030]
90. 详细化学反应模型中温度修正项特性研究 [1030]
91. 一维脉冲爆轰波的能量释放规律研究 [1026]
92. Numerical analysis of spatial evolution of the small signal gain i.. [1025]
93. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [1024]
94. 爆轰波与激波对撞爆轰状态演化机理研究 [1024]
95. 激波风洞气动力信号分离的波系适配法 [1016]
96. 超高速高焓流动研究进展 [1005]
97. Dynamic Characteristics of Spherically Converging Detonation Waves [1004]
98. 爆轰驱动高焓激波膨胀管性能研究 [1000]
99. 变截面管道中爆轰胞格演变机制的数值模拟研究 [999]
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 [989]

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 [1736]
2. On the numerical technique for the simulation of hypervelocity tes.. [1048]
3. Evolution of cellular structures on oblique detonation surfaces [961]
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.. [757]
6. Wave dynamic processes induced by a supersonic projectile discharg.. [725]
7. 高超声速高焓风洞试验技术研究进展 [604]
8. Concept of non-ablative thermal protection system for hypersonic v.. [594]
9. A reconstructed discontinuous Galerkin method based on a Hierarchi.. [589]
10. 电子发汗冷却技术及其研究进展 [556]
11. 复现飞行条件平板边界层喷流控制实验研究 [517]
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.. [495]
14. 气相爆轰物理的若干研究进展 [495]
15. 高焓流动试验装备与测试技术 [493]
16. 准定常强激波马赫反射波形结构 [484]
17. 爆轰推进概念与机理研究——新型发动机研究的热点 [450]
18. 卷积神经网络在风洞天平静态校准中的应用 [448]
19. Performance of a Detonation Driven Shock Tunnel [445]
20. JF-22超高速风洞理论基础与关键技术 [439]
21. On the transition pattern of the oblique detonation structure [436]
22. Numerical and Experimental Investigation of Wave Dynamic Processes.. [431]
23. An Integrated Evolutionary Algorithm for Expensive Global Optimiza.. [431]
24. 用FLUENT软件计算化学氧碘激光流场 [429]
25. Approximate analytic solution of heat conduction in hollow semi-sp.. [425]
26. 高超声速飞行器减阻防热研究进展 [425]
27. The Structure and Evolution of a Two-Dimensional H2/O2/Ar Cellular.. [420]
28. Numerical simulation of one-dimensional aluminum particle-air deto.. [418]
29. Shocked Flows Induced by Supersonic Projectiles Moving in Tubes [409]
30. 准定常强激波马赫反射波形的数值研究 [409]
31. 长试验时间爆轰驱动激波风洞技术研究 [408]
32. 高超声速风洞实验数据多空间相关理论与关联方法研究 [399]
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 [392]
35. Cellular Cell Bifurcation Of Cylindrical Detonations [382]
36. 一维脉冲爆轰波的能量释放规律研究 [379]
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 [374]
38. 单步化学反应模型点火延迟时间研究 [374]
39. 三维双楔面定常超声速流动研究 [370]
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 [365]
42. Numerical investigation of the reflection of unsteady decelerating.. [362]
43. Wave Propagation Analysis in a Pressure-Wave-Refrigerator [359]
44. 爆轰推进概念与机理研究——新型发动机研究的热点 [356]
45. The cellular structure of a two-dimensional H2/O2/Ar detonation wa.. [355]
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 [354]
47. 一维爆轰波不稳定性的一种理论描述 [352]
48. 爆轰驱动激波管缝合激波马赫数计算 [349]
49. Analysis of the test condition of a shock-expansion tube: JF-16 [349]
50. 模拟爆炸波的生物激波管 [348]
51. 环形激波绕射, 反射和聚焦的数值模拟研究 [347]
52. 超燃冲压发动机凹腔稳焰器非定常现象的数值研究 [344]
53. Plasma Assisted Low Temperature Combustion [343]
54. 风洞实验数据的分析与关联方法 [341]
55. 带三维凹槽火焰稳定器的燃烧室放热分布规律研究 [337]
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 [337]
57. 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]
58. Reconstructing shock front of unstable detonations based on multi-.. [335]
59. Numerical investigation on the induction zone structure of the obl.. [334]
60. 气相爆轰高速弹丸速度测量 [329]
61. Heat Transfer Problems Induced By Multi-shocks Interaction [329]
62. Micro-shock waves generated inside a fluid jet impinging on plane .. [328]
63. Numerical simulation of deflagration to detonation transition in a.. [328]
64. 爆轰波在楔面上反射数值分析 [325]
65. 超高速试验气流的建立与分析 [325]
66. 脉冲型天平高精度全自动校准系统 [325]
67. 高超声速气动热力学的几个基础研究问题 [324]
68. 高焓风洞中模型外流场电子密度测试研究 [319]
69. 基于OH自由基A2Σ + →X2Πr 电子带系发射光谱的温度测量技术 [317]
70. Abel Inversion of Axially-Symmetric Shock Wave Flows [316]
71. 激波风洞气动力信号分离的波系适配法 [316]
72. 分裂算法对准爆轰波数值模拟的影响 [316]
73. Numerical Investigation of Toroidal Shock Wave Focusing in a Cylin.. [315]
74. 无缓冲气COIL扩压器流场数值模拟 [314]
75. 详细化学反应模型中温度修正项特性研究 [313]
76. Reliable Validation Based on Optical Flow Visualization for CFD Si.. [310]
77. 脉冲爆轰发动机热射流起爆机理数值分析 [307]
78. 超高速流动实验设备和相关数值研究 [307]
79. Advances in critical technologies for hypersonic and high-enthalpy.. [305]
80. 空心半球高超声速飞行结构传热近似解析求解 [304]
81. 气相爆轰化学反应流场数值模拟 [302]
82. 高焓激波风洞喷管流场数值研究 [302]
83. Comparative study on aerodynamic heating under perfect and nonequi.. [302]
84. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [301]
85. 小尺寸自适应氢氧脉冲爆轰发动机设计和验证 [301]
86. Effects of different product phases in aluminum dust detonation mo.. [301]
87. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [299]
88. Spectral Characteristics of CN Radical (B -> X) and Its Applicatio.. [299]
89. Aerodynamic measurement of a large aircraft model in hypersonic fl.. [299]
90. 边界层对驻定斜爆轰结构和稳定性的影响 [298]
91. 先进激波风洞技术研究与进展 [298]
92. 柱面气相散心爆轰波胞格演化规律研究 [297]
93. 自由飞试验模型运动参数提取方法 [297]
94. Study on the Mechanism of Detonation to Quasi-detonation Transitio.. [295]
95. Numerical investigation on three-dimensional shock wave reflection.. [294]
96. 爆轰驱动高焓激波膨胀管研究 [291]
97. 一种激波风洞爆轰双驱动方法和装置 [291]
98. 一种爆轰驱动激波风洞卸爆装置 [289]
99. 超高速高焓流动研究进展 [288]
100. Theories and technologies for duplicating hypersonic flight condit.. [285]