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1. Flow characteristics of hypersonic inlets with different cowl-lip .. [1331]
2. 超燃冲压发动机三维尾喷管设计 [1329]
3. 三面压缩高超进气道附面层抽吸研究 [1244]
4. 气泡雾化喷嘴液雾特性 [1214]
5. 高马赫数、长时间运行发动机试车台喷管热载荷分析及冷却优化 [1152]
6. An Experimental Study of Kerosene Combustion in a Supersonic Model.. [1142]
7. 来流扰动条件下超燃冲压发动机燃烧响应数值分析 [1099]
8. Effects of entry conditions on cracked kerosene-fueled supersonic .. [1094]
9. 利用NURBS中心锥消除马赫盘的内转式进气道设计方法 [1013]
10. The vitiation effects of water vapor and carbon dioxide on the aut.. [999]
11. Theoretical analysis of effects of boundary layer bleed on scramje.. [996]
12. 超燃冲压发动机尾喷管流线追踪设计 [985]
13. 三面压缩式高超声速进气道流动结构研究 [980]
14. Numerical Study on Kerosene Spray in Supersonic Flow [948]
15. 高超声速流线追踪进气道基准流场设计 [930]
16. An Experimental Study of Kerosene Combustion in a Supersonic Model.. [928]
17. 高反压作用下二元高超声速进气道非定常流动现象研究 [916]
18. Interaction of isentropic compression waves with a bow shock [904]
19. 大内收缩比二元高超声速进气道波系配置特性 [851]
20. 高超声速长时间风洞喷管设计 [844]
21. 液体碳氢燃料超然的数值模拟 [842]
22. 高超声速进气道唇缘钝化流动的数值研究 [831]
23. 优化NURBS内转式进气道设计与流场研究 [830]
24. 局部收缩比一致的变截面高超声速内转式进气道 [804]
25. 基于激波风洞的高超声速进气道自起动测试装置 [802]
26. 扩张方式对隔离段流场特性的影响 [796]
27. 高马赫数超燃冲压发动机技术研究进展 [792]
28. 高超声速进气道唇缘钝化流动的波系配置及热负荷特性研究 [791]
29. 可变几何轴对称进气道初步设计 [788]
30. 火焰稳定器射流喷口形状对燃烧性能的影响 [787]
31. 总压特性及边界层抽吸对超燃冲压发动机推力的影响 [787]
32. 高速流动PIV示踪粒子跟随响应特性实验研究 [781]
33. 三面压缩高超进气道附面层抽吸研究 [765]
34. 超声速气流中横向煤油射流的数值模拟 [763]
35. 尾缘吹气式火焰稳定器时均流场 [753]
36. 三面压缩进气道三维激波相干研究 [738]
37. Numerical Research on Liquid Spray in Supersonic Cross Flow [715]
38. 侧压式超燃进气道流场特性研究 [706]
39. 超燃冲压发动机三维变截面尾喷管设计 [703]
40. 局部收缩比处处一致的变截面高超声速内转式进气道设计方法 [698]
41. 激波风洞进气道自起动实验方法 [695]
42. 二元高超声速进气道优化设计方法研究 [694]
43. 超燃冲压发动机实验模型设计基本问题 [686]
44. 定几何二元高超声速进气道波系配置特性 [671]
45. 污染组分对煤油燃料超燃冲压发动机性能影响分析 [652]
46. Design methodology for shape transition inlets based on constant c.. [652]
47. Study on the Near-Wake Flow behind EBMC Flameholder [648]
48. Numerical study of a fully confined supersonic slot impinging jet .. [636]
49. Iso-contraction-ratio methodology for the design of hypersonic inw.. [632]
50. 溢流槽道位置对二元高超声速进气道性能研究 [631]
51. 侧壁后切二元高超声速进气道性能研究 [604]
52. 高超声速二元进气道循环气流边界层控制方法研究 [597]
53. 带中心支板侧压进气道流场特性研究 [592]
54. Spray combustion characteristics of a gas-liquid pintle injector w.. [587]
55. Study of shock train/flame interaction and skin-friction reduction.. [584]
56. 关于Fotia隔离段流动突变理论分析的看法 [568]
57. 真实气体效应对Ma10级进气道流动的影响 [568]
58. Flow structure of pressure transmission tube and its influence on .. [567]
59. Study on the influence of expansion waves on the reflection type o.. [555]
60. 一种旋流辅助雾化且旋流度可调的气/液针栓喷注器 [554]
61. Hypergolic ignition modulated by head-on collision, intermixing an.. [550]
62. 基于动态分区概念的高超声速燃烧大涡模拟 [545]
63. 一种辐射预冷的稀薄气体捕集装置及实现方法 [533]
64. 内压缩波系对高超声速进气道自起动性能影响研究 [523]
65. 隔离段激波串非对称及震荡特性实验研究 [518]
66. Numerical investigation of mode transition and hysteresis in a cav.. [516]
67. Aerothermal characteristics of bleed slot in hypersonic flows [499]
68. 实验气体中污染组分对SCRAMJET燃烧室性能的影响 [496]
69. Numerical study on the shock/combustion interaction of oblique det.. [495]
70. 下游反压引起的激波多迟滞环分析 [491]
71. 高超声速进气道快速破膜开启的流动特性 [485]
72. Effect of cowl shock on restart characteristics of simple ramp typ.. [483]
73. Numerical study on supersonic boundary-layer transition and wall s.. [479]
74. Optical diagnostics in a detonation-driven direct-connected circul.. [475]
75. Lagrange Optimization of Shock Waves for Two-Dimensional Hypersoni.. [475]
76. Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydroge.. [471]
77. 隔离段抽吸引起的激波迟滞现象研究 [464]
78. Experimental study of mode transition characteristics of a cavity-.. [463]
79. 隔离段三维流场特性及入射激波对隔离段流场影响的研究 [454]
80. The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting .. [451]
81. 高速进气道低马赫数不起动特性及马赫数影响规律 [451]
82. 基于工程转捩模型的高超声速进气道特性 [448]
83. 一种辐射预冷的稀薄气体捕集装置 [440]
84. Simple shape model for normal shock trains in straight channels [438]
85. Performance analysis of a strut-aided hypersonic scramjet by full-.. [437]
86. 超燃冲压发动机加速过程中燃烧不稳定性研究 [431]
87. 马赫数10超燃冲压发动机燃烧室流动与传热变化特性分析 [427]
88. 单向出口的欠膨胀超声速冲击射流换热特性研究 [424]
89. Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass In.. [424]
90. Downstream pressure variation induced hysteresis in the scramjet i.. [417]
91. 全流量捕获的高超声速变截面内转式进气道快速设计方法 [417]
92. A COMPUTATIONAL MODEL FOR SPINNING EFFECTS ON POST-COLLISION VELOC.. [415]
93. 带有边界层流动控制的内转式进气道 [411]
94. 一种宽域冲压发动机自适应几何喉道燃烧室 [410]
95. Switching between symmetric and asymmetric separation-induced shoc.. [406]
96. 高马赫数燃烧强化的激波风洞试验研究 [405]
97. Numerical investigation on flow nonuniformity-induced hysteresis i.. [404]
98. 二维隔离段激波迟滞现象研究 [397]
99. Parameters for evaluating the efficiency of inlet compression [391]
100. 涡轮火箭双核心变循环发动机涵道比设计约束分析 [391]

Downloads

1. 超燃冲压发动机三维尾喷管设计 [468]
2. 气泡雾化喷嘴液雾特性 [441]
3. 一种辐射预冷的稀薄气体捕集装置及实现方法 [429]
4. Study on the influence of expansion waves on the reflection type o.. [412]
5. An Experimental Study of Kerosene Combustion in a Supersonic Model.. [407]
6. Numerical Study on Kerosene Spray in Supersonic Flow [402]
7. 优化NURBS内转式进气道设计与流场研究 [383]
8. 高超声速流线追踪进气道基准流场设计 [365]
9. Flow characteristics of hypersonic inlets with different cowl-lip .. [364]
10. Spray combustion characteristics of a gas-liquid pintle injector w.. [360]
11. Effects of entry conditions on cracked kerosene-fueled supersonic .. [344]
12. Interaction of isentropic compression waves with a bow shock [336]
13. 涡轮火箭双核心变循环发动机涵道比设计约束分析 [335]
14. 超声速气流中横向煤油射流的数值模拟 [332]
15. 三面压缩高超进气道附面层抽吸研究 [324]
16. 高超声速进气道唇缘钝化流动的波系配置及热负荷特性研究 [320]
17. Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydroge.. [318]
18. 高超声速长时间风洞喷管设计 [316]
19. 可变几何轴对称进气道初步设计 [315]
20. Numerical study on supersonic boundary-layer transition and wall s.. [305]
21. 尾缘吹气式火焰稳定器时均流场 [301]
22. 高超声速二元进气道循环气流边界层控制方法研究 [300]
23. Theoretical analysis of effects of boundary layer bleed on scramje.. [299]
24. 超燃冲压发动机尾喷管流线追踪设计 [295]
25. 局部收缩比处处一致的变截面高超声速内转式进气道设计方法 [295]
26. 大内收缩比二元高超声速进气道波系配置特性 [292]
27. An Experimental Study of Kerosene Combustion in a Supersonic Model.. [283]
28. 高马赫数、长时间运行发动机试车台喷管热载荷分析及冷却优化 [282]
29. The vitiation effects of water vapor and carbon dioxide on the aut.. [275]
30. 利用NURBS中心锥消除马赫盘的内转式进气道设计方法 [274]
31. 高反压作用下二元高超声速进气道非定常流动现象研究 [265]
32. 总压特性及边界层抽吸对超燃冲压发动机推力的影响 [258]
33. 扩张方式对隔离段流场特性的影响 [256]
34. 超燃冲压发动机实验模型设计基本问题 [253]
35. Hypergolic ignition modulated by head-on collision, intermixing an.. [249]
36. 高超声速进气道唇缘钝化流动的数值研究 [228]
37. Numerical study of a fully confined supersonic slot impinging jet .. [228]
38. 三面压缩式高超声速进气道流动结构研究 [222]
39. 基于激波风洞的高超声速进气道自起动测试装置 [219]
40. 溢流槽道位置对二元高超声速进气道性能研究 [218]
41. 侧壁后切二元高超声速进气道性能研究 [216]
42. Numerical study on the shock/combustion interaction of oblique det.. [216]
43. 三面压缩高超进气道附面层抽吸研究 [215]
44. 基于动态分区概念的高超声速燃烧大涡模拟 [211]
45. 超燃冲压发动机三维变截面尾喷管设计 [209]
46. Iso-contraction-ratio methodology for the design of hypersonic inw.. [202]
47. 火焰稳定器射流喷口形状对燃烧性能的影响 [201]
48. Numerical investigation of mode transition and hysteresis in a cav.. [200]
49. 二元高超声速进气道优化设计方法研究 [195]
50. Downstream pressure variation induced hysteresis in the scramjet i.. [189]
51. 侧压式超燃进气道流场特性研究 [188]
52. 激波风洞进气道自起动实验方法 [188]
53. Effect of cowl shock on restart characteristics of simple ramp typ.. [187]
54. 隔离段激波串非对称及震荡特性实验研究 [186]
55. 实验气体中污染组分对SCRAMJET燃烧室性能的影响 [186]
56. 局部收缩比一致的变截面高超声速内转式进气道 [185]
57. Design methodology for shape transition inlets based on constant c.. [185]
58. 定几何二元高超声速进气道波系配置特性 [183]
59. Study on the Near-Wake Flow behind EBMC Flameholder [181]
60. 反压引起的带尖楔矩形隔离段流动分离迟滞现象实验研究 [175]
61. 污染组分对煤油燃料超燃冲压发动机性能影响分析 [172]
62. 高马赫数超燃冲压发动机技术研究进展 [172]
63. 隔离段抽吸引起的激波迟滞现象研究 [171]
64. 带中心支板侧压进气道流场特性研究 [170]
65. Investigation on a truncated streamline-traced hypersonic Busemann.. [170]
66. 二维隔离段激波迟滞现象研究 [168]
67. 单向出口的欠膨胀超声速冲击射流换热特性研究 [167]
68. Reduction of surface friction drag in scramjet engine by boundary .. [165]
69. 斜爆轰波的波角和法向速度-曲率关系初步探究 [164]
70. 隔离段三维流场特性及入射激波对隔离段流场影响的研究 [163]
71. 关于Fotia隔离段流动突变理论分析的看法 [163]
72. 下游反压引起的激波多迟滞环分析 [159]
73. 基于工程转捩模型的高超声速进气道特性 [156]
74. 全流量捕获的高超声速变截面内转式进气道快速设计方法 [156]
75. Study of shock train/flame interaction and skin-friction reduction.. [154]
76. Numerical investigation on flow nonuniformity-induced hysteresis i.. [154]
77. 一种可调喷雾模式的变流量液体燃料针栓喷注器 [154]
78. 带有边界层流动控制的内转式进气道 [153]
79. Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass In.. [151]
80. Comment on "Mechanics of Combustion Mode Transition in a Direct-Co.. [150]
81. Experimental investigation of combustion-induced starting hysteres.. [148]
82. Experimental study of mode transition characteristics of a cavity-.. [147]
83. 超燃冲压发动机加速过程中燃烧不稳定性研究 [147]
84. 高超声速进气道快速破膜开启的流动特性 [140]
85. Fuel Regulation Historical Effects on Flame Stabilizations in a Ca.. [140]
86. 斜爆轰波黏性流场和起爆演化的数值研究 [140]
87. 三面压缩进气道三维激波相干研究 [139]
88. Aerothermal characteristics of bleed slot in hypersonic flows [138]
89. 真实气体效应对Ma10级进气道流动的影响 [138]
90. Design of Base Flow for Streamline-Traced Hypersonic Inlet [135]
91. Role of wall temperature on shock train in a rectangular isolator [133]
92. Lagrange Optimization of Shock Waves for Two-Dimensional Hypersoni.. [133]
93. Flow structure of pressure transmission tube and its influence on .. [132]
94. Influence of high temperature non-equilibrium effects on Mach 12 s.. [132]
95. Numerical Research on Liquid Spray in Supersonic Cross Flow [130]
96. Research on three-dimensional scramjet inlet [130]
97. 一种可承受大气动载荷的防过载补偿器 [128]
98. 高速进气道低马赫数不起动特性及马赫数影响规律 [127]
99. 高速流动PIV示踪粒子跟随响应特性实验研究 [126]
100. Switching between symmetric and asymmetric separation-induced shoc.. [126]