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1. 大庆RP-3航空煤油热物性分析 [3228]
2. 超声速燃烧与高超声速推进 [2419]
3. Heat Transfer of Aviation Kerosene at Supercritical Conditions [2257]
4. 高超声速推进热结构轻量化设计与安全评估 [1850]
5. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [1706]
6. Convective heat transfer characteristics of China RP-3 aviation ke.. [1574]
7. Development of integrated high temperature sensor for simultaneous.. [1562]
8. Analysis of Thermophysical Properties of Daqing RP-3 Aviation Kero.. [1554]
9. Study of turbulent heat transfer of aviation kerosene flows in a c.. [1533]
10. Thermal cracking of aviation kerosene for scramjet applications [1468]
11. Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Und.. [1459]
12. 一般流体的准一维定常流方程组及其在超临界碳氢燃料可压缩流动中的应用 [1456]
13. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [1406]
14. Investigation of Vaporized Kerosene Injection and Combustion in a .. [1382]
15. 热流传感器的高温标定方法的研究 [1376]
16. 高速脉冲纹影系统在超声速燃烧室内流场显示中的初步应用 [1371]
17. 超临界压力下航空煤油圆管流动和传热的数值研究 [1370]
18. Investigation of Vaporized Kerosene Injection and Combustion in a .. [1343]
19. Combustion of Vaporized Kerosene in Supersonic Model Combustors wi.. [1295]
20. 一种热流传感器 [1239]
21. 采用简化机理模拟乙烯在超声速气流中自点火燃烧过程 [1238]
22. 再生主动冷却结构耦合传热分析方法研究 [1232]
23. 脉冲纹影技术及其在超声速燃烧室流场显示中的应用 [1206]
24. 三维冷却结构中航空煤油对流传热特性实验研究 [1193]
25. A Thermal Analysis Method for Fuel-Cooled Combustor Structure base.. [1188]
26. 测量热流和温度的传感器及高温下测量热流与温度的方法 [1170]
27. Characteristics of compressible flow of supercritical kerosene [1169]
28. 超临界煤油超声速燃烧特性实验 [1157]
29. Combustion and Ignition of Thermally Cracked Kerosene in Supersoni.. [1157]
30. 超临界压力下航空煤油流动与传热特性试验 [1150]
31. Probe for Measurements of Density/Conductivity in Flows of Conduct.. [1145]
32. 主动冷却燃烧室燃烧与传热耦合过程迭代分析设计方法 [1145]
33. 带主动冷却的超声速燃烧室传热分析 [1141]
34. 气动加热对主动冷却超声速燃烧室热结构的影响 [1137]
35. 高温壁面热流与温度一体化测量传感器 [1101]
36. Effects of entry conditions on cracked kerosene-fueled supersonic .. [1091]
37. Blowout Limits of Cavity-Stabilized Flame of Supercritical Kerosen.. [1087]
38. 超临界压力下航空煤油热裂解特性研究 [1077]
39. Performance of supersonic model combustors with staged injections .. [1060]
40. 航空煤油超声速稳定燃烧贫富油极限实验研究 [1052]
41. 超临界煤油的亚/超声速喷注对超声速燃烧性能的影响实验研究 [1046]
42. 碳氢化合物超声速脉冲燃烧实验研究 [1045]
43. 超临界态煤油等熵流动和超声速喷注研究 [1039]
44. Visualization of Vaporized Kerosene Combustion in a Supersonic Com.. [1023]
45. 超声速燃烧室隔离段热环境的实验测量与理论分析 [1017]
46. 高温MEMS剪应力传感器残余应力分析 [1000]
47. 超临界压力下航空煤油水平管内对流换热特性数值研究 [996]
48. 高温壁面热流与温度一体化测量传感器研究 [981]
49. 主动冷却超燃冲压发动机燃烧室内流道设计 [965]
50. RP-3煤油热物性替代模型研究 [960]
51. 变比热效应对高焓气流总压测量的影响 [951]
52. 超声速燃烧中的特征尺度及影响因素 [945]
53. Study on Flame Stabilization in a Dual-Mode Combustor Using Optica.. [932]
54. 双路喷注超临界态煤油的超燃特性研究 [920]
55. 超临界压力下航空煤油热裂解特性研究 [920]
56. Development of Skeletal Kerosene Mechanisms and Application to Sup.. [920]
57. Performance of a Supersonic Model Combustor using Vaporized Kerose.. [916]
58. 主动冷却亚燃冲压发动机实验研究 [916]
59. 氨燃料吸气式变循环发动机性能分析 [863]
60. 超声速燃烧室热/力环境及其测量技术研究 [851]
61. Characteristic scales in supersonic combustion [850]
62. On the application of tabulated dynamic adaptive chemistry in ethy.. [834]
63. Numerical Investigation on Flame Stabilization in DLR Hydrogen Sup.. [828]
64. 同步辐射单光子电离技术研究航空煤油替代燃料环烷烃的热解反应 [824]
65. Blowout limits of supercritical kerosene in supersonic combustors [823]
66. 超临界与热裂解煤油超声速燃烧性能优化研究 [812]
67. 轻质点阵增强主动冷却壁板:设计、制备与测试 [809]
68. 超临界煤油超声速燃烧特性实验 Experiments on Supersonic Combustion.. [799]
69. 高动压超声速燃烧热防护初步分析 [799]
70. 基于涡合成方法的 可压缩入口湍流条件的生成 [775]
71. 欠膨胀声速氮气射流大涡模拟研究 [768]
72. On jet-wake flame stabilization in scramjet: A LES/RANS study from.. [760]
73. A comparative study of elliptical and round scramjet combustors by.. [754]
74. Three-Dimensional heat transfer analysis and optimized design of a.. [747]
75. 轴对称主动冷却发动机燃烧室耦合传热分析方法研究 [735]
76. 可压缩双组分混合层的直接数值模拟研究 [724]
77. 超声速燃烧场中的煤油射流结构及混合机理研究 [722]
78. Quasi-1D compressible flow of hydrocarbon fuel [717]
79. Computational realization of multiple flame stabilization modes in.. [713]
80. Development and Preliminary Validation of A Thermal Analysis Metho.. [712]
81. Characteristics of a supersonic model combustor with two-staged in.. [707]
82. 不同喷压比下欠膨胀射流对特征频率激励的响应 [707]
83. A comparative study of highly underexpanded nitrogen and hydrogen .. [699]
84. Numerical investigation of characteristic frequency excited highly.. [699]
85. Development of a radiative heating facility for studying flow and .. [697]
86. Real-gas Effect Accounted for by the Principle of Extended Corresp.. [693]
87. Full-scale Detached Eddy Simulation of kerosene fueled scramjet co.. [685]
88. 超声速燃烧数值模拟中复杂化学反应的建模方法 [680]
89. Flow characteristic of highly underexpanded jets from various nozz.. [679]
90. 一种黑体辐射标定热流计的方法 [677]
91. Comparative Study of Elliptic and Round Scramjet Combustors Fueled.. [663]
92. Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combu.. [661]
93. Measurements of the blowout limits of supercritical aviation keros.. [659]
94. A low-dissipation solver based on openFOAM designed for large eddy.. [652]
95. 一种液氧气化器装置 [645]
96. Pulsed combustion of hydrocarbon fuels in a supersonic model combu.. [639]
97. 一种高空飞行大气采样器及稀薄气体风洞实验系统 [628]
98. Evaluation and optimal design of supersonic nozzle for laser-assis.. [627]
99. An Experimental Investigation of Supersonic Combustion of Mildly C.. [626]
100. A low-dissipation scheme based on OpenFoam designed for large eddy.. [617]

Downloads

1. 大庆RP-3航空煤油热物性分析 [883]
2. Heat Transfer of Aviation Kerosene at Supercritical Conditions [872]
3. 超声速燃烧与高超声速推进 [779]
4. Analysis of Thermophysical Properties of Daqing RP-3 Aviation Kero.. [634]
5. Development of Skeletal Kerosene Mechanisms and Application to Sup.. [620]
6. 高动压超声速燃烧热防护初步分析 [553]
7. 基于涡合成方法的 可压缩入口湍流条件的生成 [544]
8. 一种高空飞行大气采样器及稀薄气体风洞实验系统 [543]
9. 氨燃料吸气式变循环发动机性能分析 [528]
10. Development of integrated high temperature sensor for simultaneous.. [490]
11. 一种使用氨工质的混合动力超声速发动机 [485]
12. Convective heat transfer characteristics of China RP-3 aviation ke.. [477]
13. 一种基于金属激光选区熔化技术的圆柱弹簧设计成形方法 [476]
14. 一种电加热空气滤芯及低能耗空气高温杀毒灭菌装置 [475]
15. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [460]
16. 超临界煤油超声速燃烧特性实验 [459]
17. Investigation of Vaporized Kerosene Injection and Combustion in a .. [438]
18. Investigation of Vaporized Kerosene Injection and Combustion in a .. [436]
19. 脉冲纹影技术及其在超声速燃烧室流场显示中的应用 [436]
20. RP-3煤油热物性替代模型研究 [430]
21. 一种吸气式火箭针栓喷注器及其喷注方法 [430]
22. A Thermal Analysis Method for Fuel-Cooled Combustor Structure base.. [428]
23. Combustion and Ignition of Thermally Cracked Kerosene in Supersoni.. [422]
24. 热流传感器的高温标定方法的研究 [420]
25. 超临界压力下航空煤油圆管流动和传热的数值研究 [398]
26. A comparative study of elliptical and round scramjet combustors by.. [387]
27. Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Und.. [382]
28. 高温壁面热流与温度一体化测量传感器 [382]
29. 超临界压力下航空煤油流动与传热特性试验 [380]
30. Study of turbulent heat transfer of aviation kerosene flows in a c.. [377]
31. 高超声速推进热结构轻量化设计与安全评估 [376]
32. 采用简化机理模拟乙烯在超声速气流中自点火燃烧过程 [371]
33. Characteristics of compressible flow of supercritical kerosene [369]
34. 主动冷却亚燃冲压发动机实验研究 [356]
35. 高温壁面热流与温度一体化测量传感器研究 [352]
36. Thermal cracking of aviation kerosene for scramjet applications [351]
37. 再生主动冷却结构耦合传热分析方法研究 [350]
38. An Experimental Investigation of Supersonic Combustion of Mildly C.. [349]
39. Effects of entry conditions on cracked kerosene-fueled supersonic .. [341]
40. 超临界压力下航空煤油热裂解特性研究 [337]
41. Visualization of Vaporized Kerosene Combustion in a Supersonic Com.. [336]
42. 主动冷却超燃冲压发动机燃烧室内流道设计 [334]
43. 三维冷却结构中航空煤油对流传热特性实验研究 [332]
44. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [332]
45. On the application of tabulated dynamic adaptive chemistry in ethy.. [332]
46. 超临界煤油的亚/超声速喷注对超声速燃烧性能的影响实验研究 [327]
47. 超声速燃烧室隔离段热环境的实验测量与理论分析 [324]
48. The role of low/high- temperature chemistry in computationally rep.. [322]
49. Blowout limits of supercritical kerosene in supersonic combustors [316]
50. 超临界与热裂解煤油超声速燃烧性能优化研究 [315]
51. 带主动冷却的超声速燃烧室传热分析 [310]
52. Comparative Study of Elliptic and Round Scramjet Combustors Fueled.. [301]
53. Flow characteristic of highly underexpanded jets from various nozz.. [300]
54. 一种热流传感器 [299]
55. Blowout Limits of Cavity-Stabilized Flame of Supercritical Kerosen.. [296]
56. 气动加热对主动冷却超声速燃烧室热结构的影响 [293]
57. Numerical Investigation on Flame Stabilization in DLR Hydrogen Sup.. [290]
58. 航空煤油超声速稳定燃烧贫富油极限实验研究 [283]
59. 一般流体的准一维定常流方程组及其在超临界碳氢燃料可压缩流动中的应用 [279]
60. Combustion of Vaporized Kerosene in Supersonic Model Combustors wi.. [279]
61. 超临界压力下航空煤油水平管内对流换热特性数值研究 [278]
62. Computational realization of multiple flame stabilization modes in.. [277]
63. Characteristic scales in supersonic combustion [276]
64. 双路喷注超临界态煤油的超燃特性研究 [272]
65. Evaluation and optimal design of supersonic nozzle for laser-assis.. [272]
66. Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combu.. [271]
67. 测量热流和温度的传感器及高温下测量热流与温度的方法 [269]
68. 主动冷却燃烧室燃烧与传热耦合过程迭代分析设计方法 [269]
69. Performance of supersonic model combustors with staged injections .. [264]
70. Probe for Measurements of Density/Conductivity in Flows of Conduct.. [263]
71. Experimental Studies of Film Cooling in Supersonic Combustors [261]
72. 高速脉冲纹影系统在超声速燃烧室内流场显示中的初步应用 [254]
73. 同步辐射单光子电离技术研究航空煤油替代燃料环烷烃的热解反应 [254]
74. 碳氢化合物超声速脉冲燃烧实验研究 [247]
75. Hypergolic ignition modulated by head-on collision, intermixing an.. [247]
76. 超声速燃烧室热/力环境及其测量技术研究 [244]
77. Numerical investigation of characteristic frequency excited highly.. [244]
78. Performance of a Supersonic Model Combustor using Vaporized Kerose.. [242]
79. 超临界态煤油等熵流动和超声速喷注研究 [239]
80. 欠膨胀声速氮气射流大涡模拟研究 [239]
81. 谐波法航空煤油热物性测量研究 [233]
82. Full-scale Detached Eddy Simulation of kerosene fueled scramjet co.. [233]
83. A comparative study of highly underexpanded nitrogen and hydrogenj.. [232]
84. Study on Flame Stabilization in a Dual-Mode Combustor Using Optica.. [231]
85. 变比热效应对高焓气流总压测量的影响 [230]
86. 超声速燃烧熄火极限实验研究 [228]
87. Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy.. [228]
88. Visualization of flow separation inside cut kerf during laser cutt.. [226]
89. 超临界压力下航空煤油热裂解特性研究 [225]
90. Large-Eddy Simulation of Time Evolution and Instability of Highly .. [225]
91. Characterization of flame stabilization modes in an ethylene-fuele.. [223]
92. Comparative Study of Elliptic and Round Scramjet Combustors Fueled.. [223]
93. Quasi-1D compressible flow of hydrocarbon fuel [218]
94. 高温MEMS剪应力传感器残余应力分析 [216]
95. 轴对称主动冷却发动机燃烧室耦合传热分析方法研究 [216]
96. 轻质点阵增强主动冷却壁板:设计、制备与测试 [214]
97. Influences of Domain Symmetry on Supersonic Combustion Modeling [214]
98. 可压缩双组分混合层的直接数值模拟研究 [209]
99. 不同喷压比下欠膨胀射流对特征频率激励的响应 [206]
100. Development and Preliminary Validation of A Thermal Analysis Metho.. [200]