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1. 大庆RP-3航空煤油热物性分析 [2036]
2. 超声速燃烧与高超声速推进 [1580]
3. Heat Transfer of Aviation Kerosene at Supercritical Conditions [1406]
4. 高超声速推进热结构轻量化设计与安全评估 [1348]
5. Analysis of Thermophysical Properties of Daqing RP-3 Aviation Kero.. [1089]
6. Convective heat transfer characteristics of China RP-3 aviation ke.. [1052]
7. 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 [1023]
8. Development of integrated high temperature sensor for simultaneous.. [955]
9. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [915]
10. Investigation of Vaporized Kerosene Injection and Combustion in a .. [865]
11. Thermal cracking of aviation kerosene for scramjet applications [849]
12. 热流传感器的高温标定方法的研究 [848]
13. 一种热流传感器 [837]
14. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [830]
15. 脉冲纹影技术及其在超声速燃烧室流场显示中的应用 [828]
16. 超临界压力下航空煤油圆管流动和传热的数值研究 [824]
17. A Thermal Analysis Method for Fuel-Cooled Combustor Structure base.. [799]
18. 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 [789]
19. 采用简化机理模拟乙烯在超声速气流中自点火燃烧过程 [774]
20. Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Und.. [769]
21. Combustion and Ignition of Thermally Cracked Kerosene in Supersoni.. [745]
22. 超临界压力下航空煤油流动与传热特性试验 [739]
23. 高温壁面热流与温度一体化测量传感器 [736]
24. 超临界压力下航空煤油热裂解特性研究 [732]
25. 带主动冷却的超声速燃烧室传热分析 [729]
26. 气动加热对主动冷却超声速燃烧室热结构的影响 [723]
27. Characteristics of compressible flow of supercritical kerosene [706]
28. 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 [704]
29. Probe for Measurements of Density/Conductivity in Flows of Conduct.. [700]
30. 超临界煤油超声速燃烧特性实验 [686]
31. 超临界态煤油等熵流动和超声速喷注研究 [686]
32. Investigation of Vaporized Kerosene Injection and Combustion in a .. [684]
33. Effects of entry conditions on cracked kerosene-fueled supersonic .. [677]
34. Performance of supersonic model combustors with staged injections .. [676]
35. 航空煤油超声速稳定燃烧贫富油极限实验研究 [675]
36. 碳氢化合物超声速脉冲燃烧实验研究 [673]
37. Study of turbulent heat transfer of aviation kerosene flows in a c.. [660]
38. 超临界压力下航空煤油水平管内对流换热特性数值研究 [659]
39. 超声速燃烧中的特征尺度及影响因素 [653]
40. 三维冷却结构中航空煤油对流传热特性实验研究 [642]
41. RP-3煤油热物性替代模型研究 [642]
42. Combustion of Vaporized Kerosene in Supersonic Model Combustors wi.. [641]
43. Blowout Limits of Cavity-Stabilized Flame of Supercritical Kerosen.. [634]
44. 高温壁面热流与温度一体化测量传感器研究 [633]
45. 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 [630]
46. 高温MEMS剪应力传感器残余应力分析 [625]
47. 超声速燃烧室隔离段热环境的实验测量与理论分析 [605]
48. Visualization of Vaporized Kerosene Combustion in a Supersonic Com.. [588]
49. 变比热效应对高焓气流总压测量的影响 [556]
50. 超声速燃烧室热/力环境及其测量技术研究 [551]
51. 双路喷注超临界态煤油的超燃特性研究 [545]
52. 超临界压力下航空煤油热裂解特性研究 [537]
53. Characteristic scales in supersonic combustion [524]
54. Performance of a Supersonic Model Combustor using Vaporized Kerose.. [516]
55. 主动冷却燃烧室燃烧与传热耦合过程迭代分析设计方法 [499]
56. 主动冷却超燃冲压发动机燃烧室内流道设计 [472]
57. 轻质点阵增强主动冷却壁板:设计、制备与测试 [471]
58. Blowout limits of supercritical kerosene in supersonic combustors [437]
59. 可压缩双组分混合层的直接数值模拟研究 [428]
60. 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 [418]
61. 超临界煤油超声速燃烧特性实验 Experiments on Supersonic Combustion.. [404]
62. Three-Dimensional heat transfer analysis and optimized design of a.. [402]
63. Quasi-1D compressible flow of hydrocarbon fuel [386]
64. 轴对称主动冷却发动机燃烧室耦合传热分析方法研究 [379]
65. Characteristics of a supersonic model combustor with two-staged in.. [379]
66. 欠膨胀声速氮气射流大涡模拟研究 [364]
67. 超声速燃烧场中的煤油射流结构及混合机理研究 [326]
68. 超临界与热裂解煤油超声速燃烧性能优化研究 [319]
69. Measurements of the blowout limits of supercritical aviation keros.. [280]
70. 一种黑体辐射标定热流计的方法 [277]
71. 碳氢燃料超声速脉冲燃烧实验研究 [274]
72. Measurements of wall heat flux and temperature in a supersonic mod.. [264]
73. 谐波法航空煤油热物性测量研究 [258]
74. Pulsed combustion of hydrocarbon fuels in a supersonic model combu.. [255]
75. Study on Flame Stabilization in a Dual-Mode Combustor Using Optica.. [251]
76. Full-scale Detached Eddy Simulation of kerosene fueled scramjet co.. [251]
77. 超声速燃烧稳燃极限的理论研究 [248]
78. 一种主动冷却亚燃冲压发动机冷却和燃烧闭环切换装置 [241]
79. 一种以加热煤油为燃料的超声速燃烧室 [232]
80. 一种液氧气化器装置 [226]
81. 不同喷压比下欠膨胀射流对特征频率激励的响应 [211]
82. 一种亚声速燃烧冲压发动机燃烧室及其再生冷却方法 [207]
83. Development and Preliminary Validation of A Thermal Analysis Metho.. [202]
84. 一种流场和火焰结构同步探测方法 [198]
85. 用于长时间超声速燃烧的空气加热装置 [197]
86. 一种用于超声速燃烧直联的异丁烷供给系统 [196]
87. 超声速燃烧实验的煤油流量控制装置 [194]
88. Numerical investigation of characteristic frequency excited highly.. [190]
89. 一种主动冷却亚燃冲压发动机燃油切换的系统和方法 [189]
90. 超临界碳氢燃料供给系统的动态频域特性研究 [189]
91. 一种采用导热标定热流计的方法 [188]
92. 基于大庆RP-3航空煤油的轴对称截面燃烧室DES模拟 [187]
93. Flow characteristic of highly underexpanded jets from various nozz.. [186]
94. 用于超声速燃烧冲压发动机试验的消声装置 [184]
95. 一种应用于超声速燃烧试验的电气设备控制电路 [182]
96. Computational realization of multiple flame stabilization modes in.. [175]
97. 一种用于主动冷却实验的辐射加热方法 [174]
98. 一种用于主动冷却实验的辐射加热系统 [170]
99. Comparative Study of Elliptic and Round Scramjet Combustors Fueled.. [170]
100. Influence of Chemical Mechanisms on Supersonic Combustion Characte.. [167]

Downloads

1. 大庆RP-3航空煤油热物性分析 [708]
2. 超声速燃烧与高超声速推进 [575]
3. Heat Transfer of Aviation Kerosene at Supercritical Conditions [463]
4. Analysis of Thermophysical Properties of Daqing RP-3 Aviation Kero.. [442]
5. 脉冲纹影技术及其在超声速燃烧室流场显示中的应用 [317]
6. A Thermal Analysis Method for Fuel-Cooled Combustor Structure base.. [314]
7. Convective heat transfer characteristics of China RP-3 aviation ke.. [302]
8. RP-3煤油热物性替代模型研究 [297]
9. 超临界压力下航空煤油热裂解特性研究 [274]
10. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [261]
11. Development of integrated high temperature sensor for simultaneous.. [258]
12. Combustion and Ignition of Thermally Cracked Kerosene in Supersoni.. [246]
13. 超临界煤油超声速燃烧特性实验 [240]
14. Investigation of Vaporized Kerosene Injection and Combustion in a .. [232]
15. 高温壁面热流与温度一体化测量传感器 [231]
16. 热流传感器的高温标定方法的研究 [228]
17. Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under.. [226]
18. 高温壁面热流与温度一体化测量传感器研究 [223]
19. Visualization of Vaporized Kerosene Combustion in a Supersonic Com.. [221]
20. Blowout Limits of Cavity-Stabilized Flame of Supercritical Kerosen.. [214]
21. 超临界压力下航空煤油流动与传热特性试验 [211]
22. Characteristics of compressible flow of supercritical kerosene [208]
23. 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 [206]
24. Study of turbulent heat transfer of aviation kerosene flows in a c.. [206]
25. 采用简化机理模拟乙烯在超声速气流中自点火燃烧过程 [200]
26. Investigation of Vaporized Kerosene Injection and Combustion in a .. [191]
27. 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 [184]
28. 一种热流传感器 [184]
29. Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Und.. [183]
30. Combustion of Vaporized Kerosene in Supersonic Model Combustors wi.. [183]
31. Characteristic scales in supersonic combustion [181]
32. 超临界压力下航空煤油水平管内对流换热特性数值研究 [179]
33. 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 [170]
34. 高超声速推进热结构轻量化设计与安全评估 [167]
35. Effects of entry conditions on cracked kerosene-fueled supersonic .. [163]
36. 超临界压力下航空煤油圆管流动和传热的数值研究 [159]
37. 三维冷却结构中航空煤油对流传热特性实验研究 [159]
38. Thermal cracking of aviation kerosene for scramjet applications [158]
39. 航空煤油超声速稳定燃烧贫富油极限实验研究 [158]
40. 超声速燃烧室热/力环境及其测量技术研究 [158]
41. 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 [157]
42. 超声速燃烧室隔离段热环境的实验测量与理论分析 [157]
43. Probe for Measurements of Density/Conductivity in Flows of Conduct.. [151]
44. 气动加热对主动冷却超声速燃烧室热结构的影响 [151]
45. 碳氢化合物超声速脉冲燃烧实验研究 [147]
46. 双路喷注超临界态煤油的超燃特性研究 [145]
47. 带主动冷却的超声速燃烧室传热分析 [143]
48. 超临界态煤油等熵流动和超声速喷注研究 [143]
49. 主动冷却超燃冲压发动机燃烧室内流道设计 [141]
50. 高温MEMS剪应力传感器残余应力分析 [132]
51. Performance of supersonic model combustors with staged injections .. [131]
52. Blowout limits of supercritical kerosene in supersonic combustors [131]
53. 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 [124]
54. 可压缩双组分混合层的直接数值模拟研究 [120]
55. 变比热效应对高焓气流总压测量的影响 [113]
56. 超临界与热裂解煤油超声速燃烧性能优化研究 [107]
57. 长时间直联式超燃试验装置 [105]
58. 主动冷却燃烧室燃烧与传热耦合过程迭代分析设计方法 [103]
59. Quasi-1D compressible flow of hydrocarbon fuel [102]
60. 超临界压力下航空煤油热裂解特性研究 [97]
61. 轻质点阵增强主动冷却壁板:设计、制备与测试 [97]
62. 轴对称主动冷却发动机燃烧室耦合传热分析方法研究 [94]
63. Characteristics of a supersonic model combustor with two-staged in.. [92]
64. 谐波法航空煤油热物性测量研究 [91]
65. 碳氢燃料超声速脉冲燃烧实验研究 [90]
66. 欠膨胀声速氮气射流大涡模拟研究 [90]
67. 超声速燃烧中的特征尺度及影响因素 [84]
68. Performance of a Supersonic Model Combustor using Vaporized Kerose.. [78]
69. 超声速燃烧场中的煤油射流结构及混合机理研究 [76]
70. Flow characteristic of highly underexpanded jets from various nozz.. [71]
71. Three-Dimensional heat transfer analysis and optimized design of a.. [69]
72. Numerical investigation of characteristic frequency excited highly.. [67]
73. 超临界煤油超声速燃烧特性实验 Experiments on Supersonic Combustion.. [65]
74. Study on Flame Stabilization in a Dual-Mode Combustor Using Optica.. [61]
75. Full-scale Detached Eddy Simulation of kerosene fueled scramjet co.. [61]
76. 超声速燃烧稳燃极限的理论研究 [59]
77. A comparative study of highly underexpanded nitrogen and hydrogen .. [54]
78. A comparative study of elliptical and round scramjet combustors by.. [54]
79. Large-Eddy Simulation of Time Evolution and Instability of Highly .. [51]
80. 基于大庆RP-3航空煤油的轴对称截面燃烧室DES模拟 [49]
81. 一种主动冷却亚燃冲压发动机燃油切换的系统和方法 [42]
82. Comparative Study of Elliptic and Round Scramjet Combustors Fueled.. [42]
83. 超临界碳氢燃料供给系统的动态频域特性研究 [41]
84. Development of a radiative heating facility for studying flow and .. [40]
85. Measurements of the blowout limits of supercritical aviation keros.. [36]
86. Measurement of heat flux distribution of supercritical kerosene fu.. [36]
87. 一种亚声速燃烧冲压发动机燃烧室及其再生冷却方法 [35]
88. Evaluation and optimal design of supersonic nozzle for laser-assis.. [35]
89. 一种液氧气化器装置 [33]
90. Experimental Studies of Film Cooling in Supersonic Combustors [33]
91. Computational realization of multiple flame stabilization modes in.. [33]
92. Pulsed combustion of hydrocarbon fuels in a supersonic model combu.. [32]
93. Visualization of flow separation inside cut kerf during laser cutt.. [32]
94. A comparative study of highly underexpanded nitrogen and hydrogenj.. [32]
95. Development of Skeletal Kerosene Mechanisms and Application to Sup.. [32]
96. 用于长时间超声速燃烧的空气加热装置 [31]
97. 一种用于超声速燃烧直联的异丁烷供给系统 [31]
98. LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combus.. [31]
99. 一种以加热煤油为燃料的超声速燃烧室 [30]
100. 超声速燃烧稳焰模式分布研究 [30]