1. Jiang ZL, Li JP, Hu ZM, et al. On theory and methods for advanced detonation-driven hypervelocity shock tunnels. National Science Review, 2020, In press

2. Jiang ZL, Hu ZM, Wang YP, Han GL. Advances in critical technologies for hypersonic and high-enthalpy wind tunnel. Chinese Journal of Aeronautics, 2020, in press

3. Yuan CK, Zhou K, Hu ZM, et al. Experimental investigation of hypervelocity flow in expansion tunnel. AIAA Journal, 2020, 58(6), 2776-2783

4. Peng J, Zhang ZJ, Hu ZM, Jiang ZL. A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections. Aerospace Science and Technology, 2019, 89:299-306

5. Fang YS, Zhang ZJ, Hu ZM, Deng X. Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures. Aerospace Science and Technology, 2019, 92:676–684

6. Fang YS, Zhang ZJ, Hu ZM. Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures. International Journal of Hydrogen Energy, 2019, 44:23429-23435

7. Yuan CK, Zhou K, Liu YF, Hu ZM, Jiang ZL. Spectral measurements of hypervelocity flow in an expansion tunnel. Acta Mechanic Sinica, 2019, 35(1):24-31

8. Luo C, Wang YP, Hu ZM, Li JP Jiang Z. Weighting by cross-validation: A calibration method for force measurements via transient response analysis, Experimental Techniques, 2019, 43:469-478

9. Fang YS, Hu ZM, Teng HH. Numerical investigation of oblique detonations induced by a finite wedge in a stoichiometric hydrogen-air mixture. Fuel, 2018, 234:502-507

10. Li XD, Hu ZM, Jiang ZL. Continuum perspective of bulk viscosity in compressible fluids. Journal of Fluid Mechanics, 2017, 812:966-990

11. Hu ZM, Zhou K, Peng J, Li JP, Jiang ZL. Shock relations in gases of heterogeneous thermodynamic properties. Science China Technological Sciences, 2017, 60:1050

12. Li XD, Hu ZM, Jiang ZL. Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile. Shock Waves, 2017, 27:771-779

13. Fang YS, Hu ZM, Teng HH, Jiang ZL, Ng HD. Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures, Aerospace Science and Technology, 2017, 71:256-263

14. Li XD, Hu ZM, Jiang ZL. Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity. Science China Technology Sciences, 2016, 59(4):1-10.

15. Wang YP, Hu ZM, Liu YF, Jiang ZL. Starting process in a large-scale shock tunnel, AIAA Journal, 2016, 54(4):1240-1249

16. Xiang GX, Wang C, Hu ZM, Li XD, Jiang ZL. Theoretical solutions to three-dimensional asymmetrical shock/shock interaction. Science China Technological Sciences, 2016, 59(8):1208-1216.

17. Jiang ZL, Wu B, Gao YL, Zhao W, Hu ZM. Development of the detonation-driven expansion tube for orbital speed experiments. Science China Technology Sciences, 2015, 58(4):695-700.

18. Hu ZM, Wang C, Jiang ZL Khoo BC. On the numerical technique for the simulation of hypervelocity test flows. Computers & Fluids, 2015, 106:12-18.

19. Luo C., Hu Z., Zhang S.-L., Jiang Z. Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles, Engineering Applications of Artificial Intelligence, 2015, 46, 93-103.

20. Luo C.T., Jiang Z., Wang C., Hu Z. Relative contribution ratio: A quantitative metrics for multi-parameter analysis, Cogent Mathematics, 2: 1068979, 2015.

21. Dou HS, Hu ZM, Khoo BC, Jiang ZL. Numerical simulation of deflagration to detonation transition in a straight duct: Effects of energy release and detonation stability. Advances in Applied Mathematics and Mechanics, 2014, 6(6): 718-731.

22. Z.M. Hu, B.C. Khoo, J.G. Zheng. The simulation of unsteady cavitating flows with external perturbations. Computers & Fluids, 2013, 77: 112-124.

23. J.G. Zheng, B.C. Khoo, Z.M. Hu. Simulation of wave-flow-cavitation interaction using a compressible homogenous flow method. Commun. Comput. Phys. 14(2):328-354, 2012.

24. Z.M. Hu, H.S. Dou, B.C. Khoo. On the modified dispersion-controlled-dissipative (DCD) scheme for computation of flow supercavitation. Computers & Fluids, 40:315-323, 2011.

25. Z.M. Hu, R.S. Myong, Y.R. Yang, T.H. Cho. Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a Ma=9 hypersonic flow. Theoretical and Computational Fluid Dynamics, 24:551-564, 2010.

26. Z.M. Hu, H.S. Dou, B.C. Khoo. Rapid detonation initiation by sparks in a short duct: a numerical study. Shock Waves, 20:241-249, 2010.

27. Z.M. Hu, Y.L. Gao, R.S. Myong, H.S. Dou, B.C. Khoo. Geometric criterion for RR？MR transition in hypersonic double-wedge flows. Physics of Fluids, 22, 016101, 2010.

28. Z.M. Hu, C. Wang, Y. Zhang, R.S. Myong. Computational confirmation of an abnormal Mach reflection configuration. Physics of Fluids, 21, 011702, 2009.

29. Z.M. Hu, R.S. Myong, M.S. Kim, T.H.Cho. Downstream flow condition effects on the RR？MR transition of asymmetric shock waves in steady flows. Journal of Fluid Mechanics, 620:43-62, 2009.

30. C. Wang, Z. Jiang, Z.M. Hu, J. Lu. Numerical Investigation on the Flowfield of “Swallowtail-type” Cavity for Supersonic Mixing Enhancement. Acta Mechanica Sinica, 25(1):37-44, 2009.

31. Z.M. Hu, M.S. Kim, R.S. Myong, T.H.Cho. On the RR？MR transition of asymmetric shock waves in steady flows: an analytical study. Shock Waves, 18:419-423, 2008.

32. Z.M. Hu, R.S. Myong, C. Wang, T.H.Cho, Z.L. Jiang. Numerical study on the oscillations induced by shock/shock interaction in hypersonic double-wedge flows. Shock Waves, 18:41-51, 2008.

33. Z.M. Hu, J.M. Lü, Z.L. Jiang, R.S. Myong, T.H Cho. Numerical study on the off-design/on-design performance of nozzle flow for supersonic chemical oxygen-iodine lasers. Acta Mechanica Sinica, 24(2):133-142, 2008.

34. Z.M. Hu, Z.L. Jiang, R.S. Myong, T.H Cho. Numerical analysis of spatial evolution of the small signal gain in a chemical oxygen-iodine laser operating without primary buffer gas. Optics and Laser Technology, 40(1):13-20, 2008.

35. C. Wang, Z. Jiang, Z.M. Hu, G.L. Han. Numerical Investigation on the Evolution of the Cylindrical Cellular Detonation. Applied Mathematics and Mechanics, 29(11):1487-1494, 2008.

36. Z.M. Hu, R.H. Myong, A.T. Nguyen, Z.L. Jiang. Numerical analysis of the flowfield in a supersonic COIL with an interleaved jet configuration and its effect on the gain distribution. Engineering Applications of Computational Fluid Mechanics, 1(3):207-215, 2007.

37. B. Deng, Z.M. Hu, H.H. Teng and Z.L. Jiang. Numerical study on cellular structure evolution of detonation in section-changing chambers. Science in China Series G: Physics, Mechanics & Astronomy, 50(6):797-808, 2007.

38. H.H. Teng, Z.L. Jiang and Z.M. Hu. Detonation initiation developing from the Richtmyer–Meshkov instability. Acta Mechanica Sinica, 23(4):343-349, 2007.

39. Z.M. Hu and Z.L. Jiang. Wave Dynamic process in cellular detonation reflection from wedges. Acta Mechanica Sinica, 23(1):33-41, 2007.

40. Z.M. Hu, R.S. Myong, T.H Cho. A robust scheme for the multi-component reactive flows in the presence of shock waves. The Korean Society of Computational Fluid Engineering, 12(1):60-67, 2007.

41. 韩子健, 彭俊, 胡宗民, 韩桂来, 姜宗林. JF-12激波风洞在火星进入环境下的运行特性研究. 航空学报, 2021, 42(3): 24129.

42. 周凯, 彭俊, 欧东斌, 胡宗民, 姜宗林. 超高速流动气动热及壁面催化效应试验研究. 中国科学技术科学，2020，in press

43. 李馨东, 赵英奎, 胡宗民, 姜宗林. 基于第二粘性的Navier-Stokes方程组求解正激波结构. 计算物理，2020，in press

44. 杨鹏飞,牟乾辉,滕宏辉,胡宗民,姜宗林. 旋转爆轰波中多波流动模式的数值研究. 推进技术, 2019, 40(2):398-406.

45. 姜宗林,李进平,胡宗民,等. 高超声速飞行复现风洞理论与方法.力学学报, 2018, 50(6):1283-1291.

46. 彭俊,张子健,周凯,胡宗民,姜宗林. 振动激发对激波反射的影响, 航空学报, 2017, 38(8):121055

47. 方宜申, 胡宗民，滕宏辉，姜宗林. 圆球诱导斜爆轰起爆的数值研究.力学学报, 2017, 49:268-273.

48. 李馨东, 赵英奎, 欧阳碧耀, 胡宗民, 姜宗林. 气体体积粘性对二维环形激波聚焦的影响, 计算物理, 2017, 34(4):394-402

49. 周凯,苑朝凯,胡宗民,姜宗林. JF-16膨胀管流场分析及升级改造. 航空学报, 2016,37(11):3296-3303.

50. 周凯,汪球,胡宗民,姜宗林. 爆轰驱动膨胀管性能研究. 航空学报, 2016,37(3):822-828.

51. 周凯,李旭东,胡宗民, 姜宗林. 超高速流动模拟及热化学反应模型对比研究. 北京航空航天大学学报, 2016, 43(6), 1173-1181.

52. 李馨东，胡宗民，姜宗林. 可压缩流体体积粘性系数的连续介质理论. 中国科学:物理 力学 天文学, 2016, 46(3):034701.

53. 汪运鹏，等，胡宗民. 长试验时间激波风洞测力技术研究，力学学报，2016，48(3), 545-556.

54. 姜宗林, 罗长童,胡宗民,刘云峰. 高超声速风洞实验数据的多维空间相关理论与关联方法. 中国科学：物理学 力学 天文学, 2015,45:034701.

55. 李康，胡宗民，姜宗林.高超声速流动上仰异常现象关键因素数值研究.中国科学：物理学 力学 天文学, 2015,45:034701.

56. 李康，胡宗民，姜宗林.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.中国科学:物理学 力学 天文学, 2015,45:044702.

57. 李康，胡宗民，姜宗林.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.力学学报, 2015, 47(2):346-350.

58. 李馨东,胡宗民,张德良,姜宗林. 一种基于AUSM思想的通量分裂方法. 计算物理，2015, 32(1): 1-12.

59. 戴旭刚,张德良,胡宗民,姜宗林.激波与爆轰波对撞的二维数值模拟, 力学学报 44(6):953-961, 2012.

60. 杨旸，姜宗林，胡宗民. 激波反射现象的研究进展.力学进展，42(2),141-161, 2012.

61. 吕俊明，胡宗民，姜宗林，王强. 基于混合发展的超声速段射流式COIL的数值优化，计算物理，27(6)：854-862，2010.

62. 吕俊明，胡宗民，王春,姜宗林. 氧碘化学激光器超声速段射流工作方式性能的数值研究，强激光与粒子束，21(9)：1305-1309，2009.

63. 王春，姜宗林，胡宗民，韩桂来. 散心柱面胞格爆轰演化数值模拟, 应用数学和力学, 29(11):1347－1354，2008.

64. 邓博, 胡宗民, 滕宏辉, 姜宗林. 变截面管道中爆轰胞格演变机制的数值模拟研究. 中国科学G 辑: 物理学 力学 天文学, 38(2): 206-216, 2008.

65. 高云亮，李进平，胡宗民，姜宗林. 准定常强激波马赫反射波的数值研究. 空气动力学报，Vol. 26(4)，456-461，2008.

66. 吕俊明，胡宗民，姜宗林: 亚声速段横向射流对Coil性能影响的数值研究，计算物理，25（4）：414－420，2008

67. 牟乾辉，胡宗民，赵伟，张德良，姜宗林. 脉冲爆轰发动机热射流起爆机制数值分析，计算物理， 23(3):266-272, 2006

68. 胡宗民，孙英英，吴宝根，姜宗林. COIL亚声速段横向喷流混合流场数值分析. 强激光与粒子束，17(4)：481-484，2005

69. 胡宗民，孙宇峰，郭长铭，张德良. 气相爆轰波传播特性的数值模拟及实验对照. 空气动力学学报,23(2):178-182，2005.

70. 刘长礼，张德良，胡宗民，姜宗林. 正向爆轰驱动高焓激波风洞的数值模拟. 计算力学学报, 22(4)：425-430，2005.

71. 常利娜，张德良，胡宗民，姜宗林. 频散可控格式的一种推广形式及其在爆轰波马赫反射中的应用. 计算物理，22(3)：189-196，2005.

72. 孙宇峰，张德良，胡宗民，姜宗林. 氢氧爆轰波在变截面扩张管道中传播的数值模拟. 爆炸与冲击，24(5)：385-390，2004.

73. 胡宗民，牟乾辉，张德良，姜宗林. 爆轰波在弯管内传播过程数值分析. 计算物理，21(5)：408－414，2004.

74. 胡宗民，高云亮，张德良，杨国伟，姜宗林. 爆轰波在楔面上反射数值分析. 力学学报，36(4):385-392，2004.

75. 胡宗民，张德良，张嘉华. 一种易于并行求解Euler方程组的分区算法. 计算力学学报，21(1)：31－37，2004.

76. 胡宗民，张德良，张嘉华. 激波在带扩容腔的变截面管中转播和消波效果的数值分析. 爆炸与冲击，23(3)：200-206，2003.

77. 胡宗民，张德良，刘长礼，姜宗林. 气相爆轰波基元反应模型数值模拟. 北京理工大学学报，23:110-115，2003.

78. 胡宗民，张德良，姜宗林. 高速列车空气动力学. 力学进展，33(3)：404-423，2003.（译）

会议发表

79. Hu ZM*, Peng J, Han ZJ, Yuan CK, Wang YP. Hypersonic flow conditions for aerodynamic tests of a Martian entry model in the shock tunnel JF12, The 32th International Symposium on Shock Waves, Jul.13~17, 2019, NUS, Singapore.

80.Ma JW, Hu ZM*, Peng J, Teng HH, Jiang ZL. Numerical investigation of hybrid detonation in aluminum particles wit h hydrogen-air mixtures, The 32th International Symposium on Shock Waves, Jul.13~17, 2019, NUS, Singapore.

81. Peng J, Hu ZM. A theoretical and numerical study of the vibration-excitation effect on the type IV shock interaction. Asia Pacific International Symposium on Aerospace Technology. Dec. 4-6, 2019, Gold Coast, Australia.

82. 方宜申,张子健,胡宗民,姜宗林. 钝楔诱导斜爆轰波起爆数值研究, 第六届爆震与新型推进学术研讨会, 2019, 婺源.

83. Zhou K, Zhang ZJ, Zhu XJ, Ou DB, Hu ZM, Jiang ZL. Hypervelocity flow visualization experiment in the JF-16 expansion tunnel. AIP Conference Proceedings 2027, 030056, 2018, The 18th International Conference on Positron Annihilation, Aug. 19-24, 2018, Florida USA.

84. Hu ZM*, Zhou K, Peng J, Jiang ZL. Hypervelocity test with a detonation driven expansion tube, The 31th International Symposium on Shock Waves, Jul.9~14, 2017, Nagoya, Japan.

85. 方宜申,胡宗民,滕宏辉,姜宗林. 均匀来流有限长楔面诱导斜爆轰波数值研究, 第十届全国流体力学学术会议, 2018, 杭州.

88. 彭俊,胡宗民,姜宗林. 火星着陆器的真实气体效应研究, 第十届全国流体力学学术会议, 2018, 杭州.

89. 马嘉文,胡宗民,滕宏辉,姜宗林. 铝粉氢气空气混合物中多相爆轰波数值模拟研究, 第十一届高超声速科学于技术会议, 2018, 长沙.

90. 方宜申,胡宗民,滕宏辉,姜宗林. 非均匀来流对斜爆轰起爆区结构的影响, 第十九届燃烧与传热传质学术交流会议, 2017, 北京.

91. 周凯,胡宗民,刘云峰,姜宗林.爆轰驱动膨胀管JF-16流场诊断及喷管设计, 北京力学会学术年会, 2016.

92. Hu ZM, Zhou K, Li JP, Jiang ZL. A theoretical solution to imperfect shock waves. The 8th Across-strait Workshop on Shock/Vortex Interaction, Hong Kong, 2016-02.

93. Wang YP, Hu ZM, Liu YF, Jiang ZL. Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel. 22nd AIAA Computational Fluid Dynamics Conference, Jun. 22-26, 2015, Dallas TX, USA.

94. Li XD, Hu ZM, Jiang ZL. A new flux splitting scheme for Euler equations of gas dynamics. AIP Conference Proceedings 1648, 850105 (2015), The international conference on numerical analysis and applied mathematics, Sep. 22-28, 2014, Rhodes, Greece.

95. 方宜申,胡宗民,滕宏辉,姜宗林.利用钝头体起爆斜爆轰的初步数值研究, 第十七届激波与激波管学术会议, 2016,成都.

96. 李馨东,胡宗民,姜宗林. 关于可压缩流体体积黏性系数的理论研究. 中国力学大会, 2015,上海.

97. 周凯,胡宗民,姜宗林. 爆轰驱动膨胀管JF-16升级改造. 中国力学大会, 2015,上海.

98. 胡宗民,周凯,姜宗林. 爆轰驱动激波膨胀管试验流场特性研究. 中国力学大会, 2015,上海.

99. 周凯,胡宗民,姜宗林,方宜申.超高速流动研究进展. 第十六届激波与激波管学术会议, 2014,洛阳.

100. 周凯,胡宗民,姜宗林. 超高速流动实验研究. 北京力学会学术年会, 2014,北京.

101. 胡宗民,席志强,李进平,姜宗林. 大型激波风洞起动流场初步分析. LHD夏季学术研讨会, 2014,北京.

102. Hu ZM, Jiang ZL. Computer-aid diagnostic of hypersonic test flow in a shock-expansion tube. The 9th Pacific Symposium on Flow Visualization and Image Processing, Aug.25-28, 2013, Busan, Korean.

103. Hu ZM, Jiang ZL. Numerical predictions for the hypervelocity test flow conditions of JF-16, The 29th International Symposium on Shock Waves, Jul.14~19, 2013, Madison, USA.

104. Hu ZM, Wang C, Jiang ZL. Thermo-chemical nonequilibrium phenomena of the strong shock wave to generate hypervelocity test flow. The 5th International Symposium on Physics of Fluids, Jun. 9~13, 2013, Jilin, China.

105. 胡宗民,姜宗林. 超高速流动研究进展, 中国力学大会, 2013.

106. 胡宗民,姜宗林. 超高速试验气流的建立与分析. 北京力学会第十九届学术年会,2013年1月, 北京.

107. 李馨东,胡宗民,姜宗林. 生物激波管的数值模拟. 北京力学会第十九届学术年会, 2013年1月, 北京.

108. Hu ZM, Wu B, Jiang ZL. Analysis of the test condition of a shock-expansion tube: JF-16. First International Conference on High Temperature Gas Dynamics, Beijing, 2012-10.

109. Hu ZM, Jiang ZL, Dou HS. Vortex generation arising from the interaction of shock wave and fuel bubble. The Sixth Across-strait Workshop on Shock/Vortex Interaction, Guiyang, 2012-07, pp: 7.

110. Z.M. Hu, X.F. Sun, Z.L. Jiang: CFD for chemically reacting flow and its applications. International Conference on Advanced Aircraft Technologies, Jinju, South Korea, May, 2012. (invited)

111. 胡宗民,李进平,姜宗林. JF16膨胀管运行条件分析的数值问题. LHD夏季学术研讨会, 2012.

112. 胡宗民,Khoo BC,姜宗林. PDE快速起爆机理数值研究. LHD夏季学术研讨会, 2011.

113. Z.M. Hu, H.S. Dou, B.C. Khoo: Flame acceleration and rapid DDT in obstructed PDE channels. Aerospace Technology Seminar, Singapore, Feb, 2011.

114. Z.M. Hu, H.S. Dou, B.C. Khoo: Numerical study on rapid detonation onset in obstructed channels with a detailed reaction model. ISWI 2010: The Shock and High Rate Properties of Matter. Cambridge, UK, Sep. 7-10, 2010.

115. Z.M. Hu, Y.R. Yang, Y. Zhang, R.S. Myong, T.H Cho. CFD confirmation of abnormal shock wave interactions. 2008 Autumn Korean Society of Computational Fluid Engineering (KSCFE) Program, Seoul, South Korea, Oct. 24, 2008.

116. Z.M. Hu, M.S. Kim, R.S. Myong, T.H Cho. Reconsideration RR？MR transition in steady flows: Symmetric vs. asymmetric reflection. 18th International Shock Interaction Symposium. Rouen, France, July 15-18, 2008.

117. Z.M. Hu, Y.R.Yang, R.S. Myong. Invisicd shock interaction: An analytical and numerical study. International Symposium on Advanced Technology for High Performance Aircraft Core parts Design. Jinju, South Korea, May 29-30, 2008.

118. Z.M. Hu, Y.R.Yang, M.S. Kim, R.S. Myong, T.H Cho. Transition phenomena of shock wave reflection in steady flows: A further analytical and numerical investigation. The 2008 KSAS Spring Conference. Peongchang, South Korea, April 17-18, 2008.

119. Z.M. Hu, Y.R.Yang, M.S. Kim, R.S. Myong, T.H Cho. Hypersonic double-wedge flows and CFD model effects. The 2007 KSAS Autumn Conference. Jeju, South Korea, November 14-17, 2007.

120. Z.M. Hu, R.S. Myong, T.H Cho. Numerical study of shock interactions in viscous, hypersonic flows over double-wedge geometries. 26th International Symposium on Shock Waves (ISSW26), G？ttingen, Germany, July 15-21, 2007.

121. 吕俊明,胡宗民,姜宗林. COIL喷管内流场与增益场的3D数值研究. 北京力学会学术年会, 2007.

122. Z.M. Hu. Numerical study on some reactive flow issues in pulse detonation engines (PDEs). 7th International Symposium on Aerospace Technology, Samcheonpo, South Korea, October, 2006.

123. 胡宗民,杨国伟,姜宗林. COIL喷管超声速段射流混合数值研究. 中国力学学会学术大会, 2005.

124. 胡宗民. 气相爆轰化学反应流场数值模拟,全国计算流体力学会议, 2004.

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