魏祥庚


的个人主页 http://teacher.nwpu.edu.cn/weixianggeng

  被浏览次数:1505

基本信息 The basic information

魏祥庚

航天学院

博士研究生毕业

博士

副教授

航空宇航科学与技术

realysnow@nwpu.edu.cn

029-88460327/13572495641

工作经历 Work Experience

200906-201305西北工业大学航天学院讲师

201306至今西北工业大学航天学院副教授 

教育经历 Education Experience

1999年-2003年,西北工业大学,本科/学士;

2003年-2009年,西北工业大学,硕博连读/硕士、博士 

教育教学 Education And Teaching

1.火箭冲压组合发动机技术

2.液体火箭发动机

3.固体火箭发动机推力调节

科学研究 Scientific Research

学术成果 Academic Achievements

1.魏祥庚,李江,金蔚,姜东,涡流阀式固体变推力集成原理样机设计与实验,固体火箭技术,2011,34(6):703~706.

2.魏祥庚,李江,陈剑,何国强,涡流阀变推力发动机涡流室涡流结构分析,固体火箭技术,2011,34(4):443~447.

3. WEI Xianggeng, LI Jiang, CHEN Jian, JIN Wei, Experimental investigation on throat insert’s thermal shock resistance using C/C composite in solid rocket motor,Advanced Materials Research, Vol.304,2011:169~174.

4. WEI Xianggeng, LI Jiang, CHEN Jian, DONG Hao, Ablation properties experiments of C/SiC throat-insert in operational environment of rocket engine, Advanced Materials Research, Vol.304, 2011:165~168.

5.魏祥庚,何国强,李江,陈剑,余晓京,控制流参数对涡流阀变推力固体发动机性能的影响,推进技术,2009,30(5):571~575.

6.魏祥庚,何国强,李江,周战锋,非同轴式喉栓变推力发动机压强响应分析,固体火箭技术,2009,32(4):409~412.

7. WEI Xiang-geng, HE Guo-qiang, LI Jiang, ZHOU Zhan-feng.The Analysis on the Rising Section of Experimental Pressure in Variable Thrust Pintle Solid Rocket Motor. 44rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, July 21-23, 2008. AIAA-2008-4604.

8. WEI Xiang-geng, HE Guo-qiang, LI Jiang, LIU Pei-jin, WANG Wen-bin.Experimental Rocket Motor Applied in Evaluate the Ablation Performance of Ablation Resistance Materials. 44rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, July 21-23, 2008. AIAA-2008-4887.

9. WEI Xiang-geng, HE Guo-qiang, LI Jiang, LIU Pei-jin, YU Xiao-jing. Experimental investigation on thrust modula-tion of SRM based on vortex valve. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati,OHIO,8-11 July 2007. AIAA-2007-5827.

10.魏祥庚,何国强,李江等,涡流阀几何参数对固体发动机推力调节特性的影响,推进技术,2007,28(4):352~355.

11. WEI Xiang-geng, HE Guo-qiang, LIU Pei-jin, LI Xiao-zhu. Experimental research on the low vulnerability of HTPB and NEPE solid propellant. 57th International Astronautical Congress. Oct.2006. Valencia,Spain. IAC-06-C4.P.2.5. 

学术文献 Academic Literature

1. 内直外旋气液同轴式喷嘴流量及雾化特性 , 2016,37(7),1280-1286 ,DOI:10.13675/j.cnki.tjjs.2016.07.011, ISSN:1001-4055
2. 复合推进剂中铝燃烧实验研究 , 2016,37(8),1579-1585 ,DOI:10.13675/j.cnki.tjjs.2016.08.023, ISSN:1001-4055
3. RBCC亚燃模态热力调节方式研究 , 2016,39(2),151-159 ,DOI:10.7673/j.issn.1006-2793.2016.02.001, ISSN:1006-2793
4. 多模态RBCC主火箭室压对引射流动燃烧影响研究 , Journal of Propulsion Technology,2016,37(6),1108-1114 ,DOI:10.13675/j.cnki.tjjs.2016.06.014, ISSN:1001-4055
5. 超-超反应混合层火焰结构与燃烧模式大涡模拟研究 , 2015,,1 ,DOI:, ISSN:
6. 西北工业大学RBCC进气道研究进展 , 2015,,1 ,DOI:, ISSN:
7. Al基粉末燃料改性方法及点火燃烧特性 , 2016,39(1),17-22,35 ,DOI:10.7673/j.issn.1006-2793.2016.01.003, ISSN:1006-2793
8. 火箭冲压组合发动机燃烧的若干基础问题研究 , 2016,30(1),1-14,27 ,DOI:10.11729/syltlx20150159, ISSN:1672-9897
9. 燃料喷注位置对于RBCC超燃模态性能的影响 , Journal of Solid Rocket Technology,2015,38(6),798-803 ,DOI:10.7673/j.issn.1006-2793.2015.06.009, ISSN:1006-2793
10. Large eddy simulation of combusiton characteristics in a hydrogen fueled model scramjet combustor , AIAA American Institute of Aeronautics and Astronautics,2015, ,DOI:, ISSN:9781624103209
11. Large eddy simulation of effects of primary rocket jet on low frequency combustion instability in a RBCC combustor , AIAA American Institute of Aeronautics and Astronautics,2015, ,DOI:, ISSN:9781624103209
12. Numerical investigation of the injection scheme for one rectangular RBCC engine at scramjet-mode , American Institute of Aeronautics and Astronautics Inc, AIAA,2015, ,DOI:, ISSN:9781624103216
13. Simulation of kerosene combustion sustaining with cavities in a strut-based RBCC engine , American Institute of Aeronautics and Astronautics Inc, AIAA,2015, ,DOI:, ISSN:9781624103216
14. HTPB和NEPE固体推进剂枪击低易损性实验研究 , 2005,25(4),714-716 ,DOI:10.3969/j.issn.1673-9728.2005.04.233, ISSN:
15. Analysis of Ablative Performance of C/C Composite Throat Containing Defects Based on X-ray 3D Reconstruction in a Solid Rocket Motor , WALTER DE GRUYTER GMBH,2015,32(4),351-359 ,DOI:10.1515/tjj-2015-0021, ISSN:0334-0082
16. 支板增强混合超声速燃烧的大涡模拟研究 , Journal of Solid Rocket Technology,2015,38(5),664-670,678 ,DOI:10.7673/j.issn.1006-2793.2015.05.012, ISSN:1006-2793
17. 考虑径向加质的固体火箭发动机内流场整体稳定性分析 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2013,36(6),727-730,747 ,DOI:10.7673/j.issn.1006-2793.2013.06.004, ISSN:1006-2793
18. 涡流阀变推力发动机推力计算方法 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2012,35(3),330-334 ,DOI:10.3969/j.issn.1006-2793.2012.03.009, ISSN:1006-2793
19. 固体火箭发动机径向加质流局部稳定性分析方法研究 , Journal of Propulsion Technology, P.O. Box 7208-26, Beijing, 100074, China,2013,34(7),925-931 ,DOI:, ISSN:1001-4055
20. 粒子流量可调的喷管烧蚀试验方法 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2008,31(1),96-98 ,DOI:10.3969/j.issn.1006-2793.2008.01.023, ISSN:1006-2793
21. 固体/液体火箭发动机环境下3DC/SiC喉衬烧蚀性能实验 , Northwestern Polytechnical University, Xi'an, 710072, China,2011,29(4),598-602 ,DOI:10.3969/j.issn.1000-2758.2011.04.018, ISSN:1000-2758
22. 涡流阀变推力发动机涡流室涡流结构分析 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2011,34(4),443-447 ,DOI:10.3969/j.issn.1006-2793.2011.04.010, ISSN:1006-2793
23. 涡流阀式固体变推力集成原理样机设计与实验 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2011,34(6),703-706 ,DOI:10.3969/j.issn.1006-2793.2011.06.007, ISSN:1006-2793
24. Analysis of vortex structure in vortex chamber of variable-thrust motor , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2011,34(4),443-447 ,DOI:, ISSN:10062793
25. Experimentally studying Ablation properties of 3D C/SiC throat-insert for solid rocket motor or liquid rocket engine , Northwestern Polytechnical University, Xi''an, 710072, China,2011,29(4),598-602 ,DOI:, ISSN:10002758
26. Design and experiment on integrated principle prototype of a solid propellant rocket motor modulated by a fluidic vortex valve , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2011,34(6),703-706 ,DOI:, ISSN:10062793
27. Subscale test method for thermal shock resistance of throat insert material , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2011,34(3),389-392 ,DOI:, ISSN:10062793
28. Missile launching velocity measurement for variable depth launch simulation experiment , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2011,34(2),265-268 ,DOI:, ISSN:10062793
29. 固冲发动机补燃室掺混流场模拟实验测量 , 2004,,231-234 ,DOI:, ISSN:
30. Experimental investigation on thrust modulation of SRM based on vortex valve , American Institute of Aeronautics and Astronautics Inc., 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, United Sta,2007,8,8152-8156 ,DOI:, ISSN:9781563479038
31. Experimental research on the low vulnerability of HTPB and NEPE solid propellant , American Institute of Aeronautics and Astronautics Inc., 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, United Sta,2006,10,6555-6561 ,DOI:, ISSN:9781605600390
32. Experimental rocket motor applied in evaluate the ablation performance of ablation resistance materials , American Institute of Aeronautics and Astronautics Inc., 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, United Sta,2008, ,DOI:, ISSN:9781563479434
33. The analysis on the rising section of experimental pressure in variable thrust pintle solid rocket motor , American Institute of Aeronautics and Astronautics Inc., 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, United Sta,2008, ,DOI:, ISSN:9781563479434
34. Numerical analysis of flow in variable thrust SRM based on vortex valve , American Institute of Aeronautics and Astronautics Inc., 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, United Sta,2007,8,7865-7870 ,DOI:, ISSN:9781563479038
35. Experimental validation of flow field in the secondary combustor of a subscale ducted rocket , Journal of Propulsion Technology,2006,27(3),205-207 ,DOI:, ISSN:10014055
36. Cold flow simulation and visualization of SDR secondary combustor inner flow field , Journal of Propulsion Technology,2005,26(5),404-407+412 ,DOI:, ISSN:10014055
37. Effects of vortex valve geometry parameters on SRM thrust modulation , Journal of Propulsion Technology, P.O. Box 7208-26, Beijing, 100074, China,2007,28(4),352-355 ,DOI:, ISSN:10014055
38. Effects of Fuel-Lean primary rocket on bypass ratio in RBCC ejector mode , American Institute of Aeronautics and Astronautics Inc.,2014, ,DOI:10.2514/6.2014-3746, ISSN:9781624103032
39. Investigation of strut-based RBCC engine configuration to improve performance in ramjet mode , American Institute of Aeronautics and Astronautics Inc.,2014, ,DOI:, ISSN:9781624102844
40. Numerical investigation of effects of boundary layer bleed on a RBCC inlet in ejector mode , American Institute of Aeronautics and Astronautics Inc., 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, United Sta,2013, ,DOI:, ISSN:9781624102226
41. Experimental study on compensating shim of tactical missile SRM in ignition impulsion , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2010,33(5),515-518 ,DOI:, ISSN:10062793
42. Numerical and experimental investigation on the RBCC engine nozzle in ejector mode , American Institute of Aeronautics and Astronautics Inc.,2014, ,DOI:, ISSN:9781624102844
43. Thrust calculation method of variable thrust SRM controlled by vortex valve , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2012,35(3),330-334 ,DOI:, ISSN:10062793
44. Experiments and numerical simulation of active cooling ceramic matrix composite , China Spaceflight Society, 2 Yuetan Beixiaojie, Beijing, 100830, China,2008,29(5),1668-1672 ,DOI:, ISSN:10001328
45. 固冲发动机补燃室掺混流场模拟实验测量 , 2004,,231-234 ,DOI:, ISSN:
46. Test method for erosion of the nozzle with adjustable particle mass flow , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2008,31(1),96-98 ,DOI:, ISSN:10062793
47. A study of analysis method for hydrodynamic stabilities of solid rocket motors with side-induced flow , Journal of Propulsion Technology, P.O. Box 7208-26, Beijing, 100074, China,2013,34(7),925-931 ,DOI:, ISSN:10014055
48. Numerical simulation and experimental verification of gas pressure wave at the exit of launching tube , Northwestern Polytechnical University, Xi''an, 710072, China,2011,29(3),497-502 ,DOI:, ISSN:10002758
49. Ablation test for tailpipe nozzle of solid rocket motor , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2010,33(1),34-35+40 ,DOI:, ISSN:10062793
50. Effects of control flow parameters on vortex valve SRM thrust modulation , Journal of Propulsion Technology, P.O. Box 7208-26, Beijing, 100074, China,2009,30(5),571-575 ,DOI:, ISSN:10014055
51. Analysis on response of pressure in non-coaxial variable thrust pintle motor , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2009,32(4),409-412 ,DOI:, ISSN:10062793
52. Experimental investigation of erosion performance of pintle in thrust-controllable SRM , Journal of Solid Rocket Technology, P.O. Box 120, Xi''an, 710025, China,2009,32(2),163-166+170 ,DOI:, ISSN:10062793
53. Calculating effects of relevant parameters on vortex valve control of variable thrust SRM , Northwestern Polytechnical University, Xi''an, 710072, China,2009,27(2),178-183 ,DOI:, ISSN:10002758
54. RBCC燃烧室超声速反应混合层特性的大涡模拟 , China Spaceflight Society,2015,36(8),940-946 ,DOI:10.3873/j.issn.1000-1328.2015.08.011, ISSN:1000-1328
55. 变深度模拟发射实验导弹出简速度测量方法 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2011,34(2),265-268 ,DOI:10.3969/j.issn.1006-2793.2011.02.029, ISSN:1006-2793
56. 战术导弹固体火箭发动机补偿垫点火冲击动态过程的实验研究 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2010,33(5),515-518 ,DOI:10.3969/j.issn.1006-2793.2010.05.008, ISSN:1006-2793
57. 固体火箭发动机长尾喷管烧蚀实验研究 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2010,33(1),34-35,40 ,DOI:10.3969/j.issn.1006-2793.2010.01.009, ISSN:1006-2793
58. 非同轴式喉栓变推力发动机压强响应分析 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2009,32(4),409-412 ,DOI:10.3969/j.issn.1006-2793.2009.04.013, ISSN:1006-2793
59. 涡流阀式变推力发动机性能影响因素数值研究 , Northwestern Polytechnical University, Xi'an, 710072, China,2009,27(2),178-183 ,DOI:10.3969/j.issn.1000-2758.2009.02.007, ISSN:1000-2758
60. 变推力固体火箭发动机喉栓烧蚀试验研究 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2009,32(2),163-166,170 ,DOI:10.3969/j.issn.1006-2793.2009.02.011, ISSN:1006-2793
61. 涡流阀几何参数对固体发动机推力调节特性的影响 , Journal of Propulsion Technology, P.O. Box 7208-26, Beijing, 100074, China,2007,28(4),352-355 ,DOI:10.3321/j.issn:1001-4055.2007.04.004, ISSN:1001-4055
62. 固冲发动机补燃室流场的实验校测 , Journal of Propulsion Technology,2006,27(3),205-207 ,DOI:10.3321/j.issn:1001-4055.2006.03.004, ISSN:1001-4055
63. 固冲补燃室内流场冷流模拟及显示 , Journal of Propulsion Technology,2005,26(5),404-407,412 ,DOI:10.3321/j.issn:1001-4055.2005.05.006, ISSN:1001-4055
64. 控制流参数对涡流阀变推力固体发动机性能的影响 , Journal of Propulsion Technology, P.O. Box 7208-26, Beijing, 100074, China,2009,30(5),571-575 ,DOI:, ISSN:1001-4055
65. 耐高温复合材料的主动冷却实验和数值计算研究 , China Spaceflight Society, 2 Yuetan Beixiaojie, Beijing, 100830, China,2008,29(5),1668-1672 ,DOI:10.3873/j.issn.1000-1328.2008.05.039, ISSN:1000-1328
66. 某型发射动力系统缩比试验方法研究 , 2011,31(2),60-62,152 ,DOI:10.3969/j.issn.1673-9728.2011.02.018, ISSN:1673-9728
67. 水下发射筒口气幕上下边界计算方法研究 , 2010,30(6),165-167 ,DOI:10.3969/j.issn.1673-9728.2010.06.050, ISSN:1673-9728
68. 空空导弹多脉冲固体火箭发动机能量分配优化研究 , 2010,30(6),144-146 ,DOI:10.3969/j.issn.1673-9728.2010.06.043, ISSN:1673-9728
69. 全球定位系统的 L5信号的跟踪分析研究 , 2007,27(3),95-98 ,DOI:10.3969/j.issn.1673-9728.2007.03.029, ISSN:
70. Ignition and Combustion of Magnesium Particles in Carbon Dioxide , TRANS TECH PUBLICATIONS LTD,2012,152-154,220-225 ,DOI:10.4028/www.scientific.net/AMM.152-154.220, ISSN:1660-9336
71. Affective Factors Investigation on Variable Thrust Pintle Motor Performance , NORTHWESTERN POLYTECHNICAL UNIVERSITY PRESS,2010,,1064-1067 ,DOI:, ISSN:
72. 一种用于固体推进剂燃速的测试装置及测试方法 , 2014, ,DOI:, ISSN:
73. 一种火箭基组合循环发动机变工况一次火箭系统 , 2014, ,DOI:, ISSN:
74. 高压环境中Mg/CO2点火燃烧性能分析 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2013,36(3),342-345 ,DOI:10.7673/j.issn.1006-2793.2013.03.011, ISSN:1006-2793
75. 一种火箭基组合循环发动机变结构尾喷管 , 2014, ,DOI:, ISSN:
76. 一种测量高压下层流预混火焰传播速度的实验系统 , 2014, ,DOI:, ISSN:
77. 一种火箭基组合循环发动机变结构进气道 , 2014, ,DOI:, ISSN:
78. 一种火箭基组合循环引射模态性能实验发动机 , 2014, ,DOI:, ISSN:
79. 一种在实现物理隔离的计算机之间交换信息的方法 , 2014, ,DOI:, ISSN:
80. 一种用于提高RBCC双模态燃烧室掺混燃烧的燃料支板 , 2013, ,DOI:, ISSN:
81. 一种火箭基组合动力循环发动机引射火箭T型布局 , 2013, ,DOI:, ISSN:
82. 一种圆形结构的中心火箭式双模态冲压发动机 , 2011, ,DOI:, ISSN:
83. 一种固体火箭发动机全尺寸喷管热结构实验装置 , 2010, ,DOI:, ISSN:
84. 一种研究喷嘴喷注雾化特性的实验装置 , 2010, ,DOI:, ISSN:
85. 一种恒流式时序控制点火装置 , 2010, ,DOI:, ISSN:
86. 一种恒流式时序控制点火装置及控制方法 , 2010, ,DOI:, ISSN:
87. 一种实时识别固体火箭发动机燃烧结束的方法 , 2010, ,DOI:, ISSN:
88. 一种喷射式消除燃烧振荡的冲压发动机燃烧室 , 2009, ,DOI:, ISSN:
89. 一种抽吸式消除燃烧振荡的吸气式发动机燃烧室 , 2009, ,DOI:, ISSN:
90. 组合喷孔燃气流体控制阀 , 2008, ,DOI:, ISSN:
91. 直进单孔燃气流体控制阀 , 2008, ,DOI:, ISSN:
92. Large eddy simulation of flame structure and combustion mode in a hydrogen fueled supersonic combustor , PERGAMON-ELSEVIER SCIENCE LTD,2015,40(31),9815-9824 ,DOI:10.1016/j.ijhydene.2015.06.011, ISSN:0360-3199
93. 发射筒口燃气压力波数值模拟及实验验证 , Northwestern Polytechnical University, Xi'an, 710072, China,2011,29(3),497-502 ,DOI:10.3969/j.issn.1000-2758.2011.03.032, ISSN:1000-2758
94. Experimental investigation on throat insert's thermal shock resistance using C/C composite in solid rocket motor , TRANS TECH PUBLICATIONS LTD,2011,304,169-174 ,DOI:10.4028/www.scientific.net/AMR.304.169, ISSN:1022-6680
95. Ablation properties experiments of C/SiC throat-insert in operational environment of rocket engine , TRANS TECH PUBLICATIONS LTD,2011,304,165-168 ,DOI:10.4028/www.scientific.net/AMR.304.165, ISSN:1022-6680
96. Numerical Study of a Boundary Layer Bleed for a Rocket-Based Combined-Cycle Inlet in Ejector Mode , WALTER DE GRUYTER GMBH,2014,31(4),347-359 ,DOI:10.1515/tjj-2014-0006, ISSN:0334-0082
97. 喉衬材料抗热震性能缩比考核试验方法 , Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China,2011,34(3),389-392 ,DOI:10.3969/j.issn.1006-2793.2011.03.026, ISSN:1006-2793
98. RBCC发动机主被动复合热防护方案研究 , Journal of Solid Rocket Technology,2015,38(2),185-191 ,DOI:10.7673/j.issn.1006-2793.2015.02.007, ISSN:1006-2793
99. 基于BDP模型的AP/HTPB推进剂燃速参数敏感性分析 , Journal of Solid Rocket Technology,2015,38(2),245-250 ,DOI:10.7673/j.issn.1006-2793.2015.02.017, ISSN:1006-2793
100. HTPB和NEPE固体推进剂枪击低易损性实验研究 , 2005,(中国四川成都),3 ,DOI:, ISSN:
101. 基于EASY5的液发系统建模与仿真可行性研究 , 2015,41(1),70-75 ,DOI:, ISSN:1672-9374

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