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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 [3818]
2. On the numerical technique for the simulation of hypervelocity tes.. [1943]
3. 准定常强激波马赫反射波形的数值研究 [1535]
4. 准定常强激波马赫反射波形结构 [1434]
5. 高超声速流动上仰异常现象关键因素数值研究 [1307]
6. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [1278]
7. 爆轰波在楔面上反射数值分析 [1149]
8. 爆轰波在楔面上反射数值分析 [1144]
9. 超高速试验气流的建立与分析 [1139]
10. 脉冲爆轰发动机热射流起爆机理数值分析 [1128]
11. 爆轰波在弯管内传播过程数值分析 [1118]
12. 斜爆轰发动机进气道喷注系统混合特性研究 [1105]
13. Analysis of the test condition of a shock-expansion tube: JF-16 [1098]
14. 气相爆轰化学反应流场数值模拟 [1066]
15. 正向爆轰驱动高焓激波风洞的数值模拟 [1052]
16. 一种基于AUSM思想的通量分裂方法 [1051]
17. Numerical simulation of deflagration to detonation transition in a.. [1038]
18. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [1034]
19. Numerical analysis of spatial evolution of the small signal gain i.. [1031]
20. 爆轰波与激波对撞爆轰状态演化机理研究 [1025]
21. 变截面管道中爆轰胞格演变机制的数值模拟研究 [1001]
22. 激波在带扩容室的变截面管中传播和消波效果的数值分析 [995]
23. 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]
24. 散心柱面胞格爆轰演化数值研究 [978]
25. 钝锥模型高焓流动的再压缩效应研究 [973]
26. 超声速圆柱尾流及其稳定性的数值模拟 [952]
27. 风洞实验数据的分析与关联方法 [927]
28. Numerical Investigation On Evolution Of Cylindrical Cellular Deton.. [921]
29. Numerical Investigation On Detonation Cell Evolution In A Channel .. [917]
30. Vortex generation arising from the interaction of shock wave and f.. [916]
31. 激波反射现象的研究进展 [907]
32. 强化超声速混合的三维“燕尾”型壁面凹槽流动特性数值研究 [904]
33. 高超声速风洞实验数据分析与关联的几种新方法 [901]
34. 气相爆轰波传播特性的数值模拟及实验对照 [897]
35. NUMERICAL ANALYSIS OF THE FLOWFIELD IN A SUPERSONIC COIL WITH AN I.. [890]
36. 模拟爆炸波的生物激波管 [889]
37. 超高速流动实验设备和相关数值研究 [889]
38. 一种易于并行求解Euler方程组的分区技术 [872]
39. Development of the detonation-driven expansion tube for orbital sp.. [862]
40. COIL亚声速段横向喷流混合流场数值分析 [843]
41. 长试验时间激波风洞测力技术研究 [834]
42. 氧碘化学激光器超声速段射流工作方式性能的数值研究 [820]
43. Continuum perspective of bulk viscosity in compressible fluids [817]
44. COIL新体系混合与反应流场数值研究 [785]
45. CFD for chemically reacting flow and its applications [780]
46. 壁面催化效应对高超声速气动热影响研究 [777]
47. 氢氧爆轰波在变截面扩张管道中传播的数值模拟 [773]
48. 摄动有限差分方法及其应用 [767]
49. 基于混合发展的超声速段射流式COIL的数值优化 [767]
50. 生物激波管的数值模拟 [746]
51. 亚声速段横向射流对Coil性能影响的数值研究 [745]
52. Theoretical solutions to three-dimensional asymmetrical shock/shoc.. [729]
53. 混合格式在高超声速气动热模拟中的特性研究 [719]
54. 圆球诱发斜爆轰波的数值研究 [706]
55. PDE快速起爆机理数值研究 [704]
56. 爆轰驱动膨胀管性能研究 [702]
57. 流体第二粘性的连续介质模型及其物理内涵 [699]
58. Numerical investigation of oblique detonations induced by a finite.. [698]
59. Transition Between Detonation and Deflagration in a Tube with a Ca.. [696]
60. A New Flux Splitting Scheme for Euler Equations of Gas Dynamics [676]
61. Numerical investigation of the effects of shock tube geometry on t.. [675]
62. 气相爆轰波基元反应模型数值模拟 [671]
63. 基于机器学习预测激波相互作用位置的研究 [666]
64. Adaptive space transformation: An invariant based method for predi.. [665]
65. JF16 膨胀管运行条件分析的数值问题 [662]
66. 高超声速飞行复现风洞理论与方法 [659]
67. Starting Process in a Large-Scale Shock Tunnel [658]
68. Initiation of oblique detonation waves induced by a blunt wedge in.. [652]
69. 超高速流动研究进展 [637]
70. 壁面催化效应数值研究 [629]
71. Parameter-correlation study on shock-shock interaction using a mac.. [622]
72. Advances in critical technologies for hypersonic and high-enthalpy.. [609]
73. Numerical study of inflow equivalence ratio inhomogeneity on obliq.. [602]
74. Starting Process in a Large-Scale Shock Tunnel [599]
75. 关于可压缩流体体积黏性系数的理论研究 [585]
76. 气体体积粘性对二维环形激波聚焦的影响 [585]
77. 斜爆轰波系在受限空间内的演变及其临界条件的数值研究 [570]
78. Spectral measurements of hypervelocity flow in an expansion tunnel [567]
79. JF-16膨胀管流场分析及升级改造 [563]
80. JF-22超高速风洞理论基础与关键技术 [560]
81. 旋转爆轰波中多波流动模式的数值研究 [557]
82. 不同参数对气动性能影响程度的量化评价方法 [556]
83. Numerical investigation on the thermal protection mechanism for bl.. [555]
84. A theoretical and computational study of the vibration excitation .. [554]
85. 第二粘性对“真实激波的形成与结构”的影响研究 [553]
86. 超高速流动模拟及热化学反应模型对比研究 [551]
87. F12激波风洞测力技术研究 [550]
88. Computational Confirmation of AN Abnormal Mach Reflection Wave Con.. [543]
89. 振动激发对激波反射的影响 [542]
90. Numerical investigations of the lateral heat transfer in coaxial t.. [539]
91. 可压缩流体体积黏性的连续介质理论 [528]
92. 基于第二粘性的Navier-Stokes方程组求解正激波结构 [528]
93. On theory and methods for advanced detonation-driven hypervelocity.. [527]
94. Weighting by Cross-Validation: A Calibration Method for Force Meas.. [525]
95. JF-12激波风洞在火星进入环境下的运行特性 [525]
96. Shock relations in gases of heterogeneous thermodynamic properties [519]
97. 复现高超声速飞行条件激波风洞研究集体 [514]
98. 高焓热化学非平衡流动中再压缩效应对球-锥气动力的影响 [513]
99. Detonation initiation developing from the Richtmyer-Meshkov instab.. [498]
100. Effects of boundary layer on wedge-induced oblique detonation stru.. [487]

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 [1742]
2. On the numerical technique for the simulation of hypervelocity tes.. [1055]
3. 壁面催化效应对高超声速气动热影响研究 [506]
4. 准定常强激波马赫反射波形结构 [486]
5. JF-22超高速风洞理论基础与关键技术 [465]
6. 准定常强激波马赫反射波形的数值研究 [414]
7. 正向爆轰驱动高焓激波风洞的数值模拟 [394]
8. 超声速圆柱尾流及其稳定性的数值模拟 [370]
9. 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]
10. Analysis of the test condition of a shock-expansion tube: JF-16 [353]
11. 模拟爆炸波的生物激波管 [350]
12. 风洞实验数据的分析与关联方法 [342]
13. Numerical simulation of deflagration to detonation transition in a.. [335]
14. 爆轰波在楔面上反射数值分析 [327]
15. 超高速试验气流的建立与分析 [327]
16. 气相爆轰波传播特性的数值模拟及实验对照 [323]
17. 气相爆轰化学反应流场数值模拟 [310]
18. Wave Dynamic Processes in Cellular Detonation Reflection from Wedg.. [309]
19. 超高速流动实验设备和相关数值研究 [309]
20. 脉冲爆轰发动机热射流起爆机理数值分析 [308]
21. Advances in critical technologies for hypersonic and high-enthalpy.. [305]
22. Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence .. [302]
23. 高超声速流动上仰异常现象关键因素数值研究 [287]
24. 激波在带扩容室的变截面管中传播和消波效果的数值分析 [286]
25. Numerical Investigation On Detonation Cell Evolution In A Channel .. [285]
26. 爆轰波与激波对撞爆轰状态演化机理研究 [275]
27. 钝锥模型高焓流动的再压缩效应研究 [271]
28. 高超声速风洞实验数据分析与关联的几种新方法 [269]
29. Continuum perspective of bulk viscosity in compressible fluids [254]
30. A New Flux Splitting Scheme for Euler Equations of Gas Dynamics [253]
31. 混合格式在高超声速气动热模拟中的特性研究 [242]
32. NUMERICAL ANALYSIS OF THE FLOWFIELD IN A SUPERSONIC COIL WITH AN I.. [240]
33. Numerical analysis of spatial evolution of the small signal gain i.. [237]
34. 爆轰波在楔面上反射数值分析 [235]
35. 氢氧爆轰波在变截面扩张管道中传播的数值模拟 [234]
36. 氧碘化学激光器超声速段射流工作方式性能的数值研究 [229]
37. Numerical investigation of the effects of shock tube geometry on t.. [229]
38. Development of the detonation-driven expansion tube for orbital sp.. [228]
39. Starting Process in a Large-Scale Shock Tunnel [228]
40. 流体第二粘性的连续介质模型及其物理内涵 [228]
41. 强化超声速混合的三维“燕尾”型壁面凹槽流动特性数值研究 [217]
42. Numerical investigation on the thermal protection mechanism for bl.. [213]
43. Initiation of oblique detonation waves induced by a blunt wedge in.. [211]
44. 变截面管道中爆轰胞格演变机制的数值模拟研究 [210]
45. 爆轰波在弯管内传播过程数值分析 [208]
46. Theoretical solutions to three-dimensional asymmetrical shock/shoc.. [208]
47. Spectral measurements of hypervelocity flow in an expansion tunnel [206]
48. Numerical Investigation On Evolution Of Cylindrical Cellular Deton.. [203]
49. 摄动有限差分方法及其应用 [203]
50. 散心柱面胞格爆轰演化数值研究 [201]
51. 一种易于并行求解Euler方程组的分区技术 [200]
52. Starting Process in a Large-Scale Shock Tunnel [199]
53. JF16 膨胀管运行条件分析的数值问题 [198]
54. CFD for chemically reacting flow and its applications [196]
55. JF-16膨胀管流场分析及升级改造 [196]
56. Weighting by Cross-Validation: A Calibration Method for Force Meas.. [192]
57. On theory and methods for advanced detonation-driven hypervelocity.. [190]
58. 旋转爆轰波中多波流动模式的数值研究 [188]
59. 超高速流动研究进展 [185]
60. 气体体积粘性对二维环形激波聚焦的影响 [182]
61. Vortex generation arising from the interaction of shock wave and f.. [181]
62. Parameter-correlation study on shock-shock interaction using a mac.. [181]
63. 激波反射现象的研究进展 [180]
64. 生物激波管的数值模拟 [180]
65. 不同参数对气动性能影响程度的量化评价方法 [180]
66. COIL亚声速段横向喷流混合流场数值分析 [179]
67. 振动激发对激波反射的影响 [178]
68. Hypervelocity Test with a Detonation-Driven Expansion Tube [178]
69. 亚声速段横向射流对Coil性能影响的数值研究 [177]
70. Shock relations in gases of heterogeneous thermodynamic properties [177]
71. 圆球诱发斜爆轰波的数值研究 [177]
72. Adaptive space transformation: An invariant based method for predi.. [175]
73. Numerical analysis on wave dynamic processes in pulse detonation d.. [174]
74. Numerical investigation of oblique detonations induced by a finite.. [174]
75. Numerical study of the oscillations induced by shock/shock interac.. [173]
76. Numerical study of inflow equivalence ratio inhomogeneity on obliq.. [172]
77. 高超声速风洞气动力/热试验数据天地相关性研究进展 [165]
78. Transition Between Detonation and Deflagration in a Tube with a Ca.. [163]
79. 超高速流动气动热及壁面催化效应试验研究 [162]
80. 基于混合发展的超声速段射流式COIL的数值优化 [161]
81. 高焓热化学非平衡流动中再压缩效应对球-锥气动力的影响 [160]
82. 爆轰驱动膨胀管JF-16流场诊断及喷管设计 [160]
83. PDE快速起爆机理数值研究 [158]
84. 一种基于AUSM思想的通量分裂方法 [158]
85. Numerical Study on the Performance of Nozzle Flow for Supersonic C.. [155]
86. 关于可压缩流体体积黏性系数的理论研究 [152]
87. 高超声速风洞实验数据的多维空间相关理论与关联方法 [151]
88. 爆轰驱动膨胀管性能研究 [148]
89. Numerical investigations of the lateral heat transfer in coaxial t.. [148]
90. Effects of boundary layer on wedge-induced oblique detonation stru.. [146]
91. Computational Confirmation of AN Abnormal Mach Reflection Wave Con.. [144]
92. 同轴热电偶瞬态热流传感器氧化式绝缘层加工制作装置 [143]
93. 一种求解Euler方程组的新通量分裂方法 [139]
94. 基于第二粘性的Navier-Stokes方程组求解正激波结构 [139]
95. 【释疑解惑】漫说航天器回地之路 [139]
96. A theoretical and computational study of the vibration excitation .. [138]
97. JF-12激波风洞在火星进入环境下的运行特性 [138]
98. 爆轰驱动激波膨胀管试验流场特性研究 [137]
99. 高超声速飞行复现风洞理论与方法 [136]
100. 一种爆轰驱动激波风洞的双向爆轰驱动方法 [134]