基本信息
李新亮 男 博导 力学研究所
电子邮件:lixl@imech.ac.cn
通信地址:北京市海淀区北四环西路15号,中国科学院力学研究所
邮政编码:100190

研究领域

飞行器可压缩湍流与转捩;
计算流体力学;
空气动力学

招生信息

   
招生专业
080103-流体力学
081202-计算机软件与理论
招生方向
流体力学
高性能计算

教育背景

   
学历
1990-1994于吉林大学数学系应用力学专业,本科;
1994-1997于吉林大学数学研究所计算力学专业,硕士;
1997-2000年于中国科学院力学研究所,博士;
学位
力学所 理学博士学位(2000.08.28)
出国学习工作
2005年8月-2007年8月在日本东京工业大学做JSPS特别研究员

工作经历

   
社会兼职
2013-06--今 Computer and Fluids 杂志编委
2013-06--今 中科院超级计算用户委员会委员
2011-07--今 中国空气动力学会物理力学专业委员会副主任委员
2002-08--今 计算物理》杂志编委
2002-08--今 计算物理学会常务理事

教授课程

计算流体力学

专利与奖励

2000年度中国科学院自然科学二等奖(第3完成人)
奖励信息
(1) 可压缩湍流直接数值模拟,二等奖,部委级,2000

出版信息

   
发表论文
[1] Fulin TONG, Junyi DUAN, Xinliang LI. Characteristics of reattached boundary layer in shock wave and turbulent boundary layer interaction. Chinese Journal of Aeronautics. 2022, 35(6): 172-185, [2] Tong, Fulin, Duan, Junyi, Li, Xinliang. Characteristics of wall-shear stress fluctuations in shock wave and turbulent boundary layer interaction. JOURNAL OF TURBULENCE[J]. 2021, 22(12): 761-783, http://dx.doi.org/10.1080/14685248.2021.1974466.
[3] Qi, Han, Li, Xinliang, Yu, Changping. Subgrid-scale helicity equation model for large-eddy simulation of turbulent flows. PHYSICS OF FLUIDS[J]. 2021, 33(3): https://www.webofscience.com/wos/woscc/full-record/WOS:000629011300007.
[4] Tong, Fulin, Sun, Dong, Li, Xinliang. Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall. CHINESE JOURNAL OF AERONAUTICS[J]. 2021, 34(5): 350-363, http://dx.doi.org/10.1016/j.cja.2020.10.016.
[5] He, Kang, Liu, Hongwei, Li, Xinliang. A hybrid kinetic WGVC-WENO scheme for compressible flows. COMPUTERS & FLUIDS[J]. 2021, 229: http://dx.doi.org/10.1016/j.compfluid.2021.105092.
[6] Tong, Fulin, Duan, Junyi, Li, Xinliang. Shock wave and turbulent boundary layer interaction in a double compression ramp. COMPUTERS & FLUIDS[J]. 2021, 229: http://dx.doi.org/10.1016/j.compfluid.2021.105087.
[7] Tong, Fulin, Sun, Dong, Li, Xinliang. Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall. NEUROPSYCHIATRIC DISEASE AND TREATMENT[J]. 2021, 17: 350-363, http://dx.doi.org/10.1016/j.cja.2020.10.0161000-9361.
[8] Duan, Junyi, Li, Xin, Li, Xinliang, Liu, Hongwei. Direct numerical simulation of a supersonic turbulent boundary layer over a compression-decompression corner. PHYSICS OF FLUIDS[J]. 2021, 33(6): http://dx.doi.org/10.1063/5.0052453.
[9] Kang, Jian, Li, Xinliang. A Sufficient and Necessary Condition of the Existence of WENO-Like Linear Combination for Finite Difference Schemes. COMMUNICATIONS IN COMPUTATIONAL PHYSICS[J]. 2021, 29(2): 534-570, http://dx.doi.org/10.4208/cicp.OA-2019-0112.
[10] Li, Xinliang, Fu, Yaowei, Yu, Changping, Li, Li. Statistical characteristics of turbulent mixing in spherical and cylindrical converging Richtmyer-Meshkov instabilities. JOURNAL OF FLUID MECHANICS[J]. 2021, 928: [11] Xu, Dehao, Wang, Jianchun, Wan, Minping, Yu, Changping, Li, Xinliang, Chen, Shiyi. Compressibility effect in hypersonic boundary layer with isothermal wall condition. PHYSICAL REVIEW FLUIDS[J]. 2021, 6(5): http://dx.doi.org/10.1103/PhysRevFluids.6.054609.
[12] Yan, Zheng, Li, Xinliang, Yu, Changping, Wang, Jianchun, Chen, Shiyi. Dual channels of helicity cascade in turbulent flows. JOURNAL OF FLUID MECHANICS[J]. 2020, 894: https://www.webofscience.com/wos/woscc/full-record/WOS:000529155000001.
[13] Yan, Zheng, Li, Xinliang, Yu, Changping. Scale locality of helicity cascade in physical space. PHYSICS OF FLUIDS[J]. 2020, 32(6): https://www.webofscience.com/wos/woscc/full-record/WOS:000542742100001.
[14] Tong, Fulin, Chen, Jianqiang, Sun, Dong, Li, Xinliang. Wall-shear stress fluctuations in a supersonic turbulent boundary layer over an expansion corner. JOURNAL OF TURBULENCE[J]. 2020, 21(7): 355-374, https://www.webofscience.com/wos/woscc/full-record/WOS:000551328100001.
[15] Fu, Yaowei, Yu, Changping, Li, Xinliang. Energy transport characteristics of converging Richtmyer-Meshkov instability. AIP ADVANCES[J]. 2020, 10(10): https://doaj.org/article/8a09c2429bb64d6e822a6d6a04b66b3f.
[16] 童福林, 周桂宇, 孙东, 李新亮. 膨胀效应对激波/湍流边界层干扰的影响. 航空学报[J]. 2020, 41(9): 38-52, http://lib.cqvip.com/Qikan/Article/Detail?id=7102996204.
[17] Yan, Zheng, Li, Xinliang, Yu, Changping, Wang, Jianchun. Cross-chirality transfer of kinetic energy and helicity in compressible helical turbulence. PHYSICAL REVIEW FLUIDS[J]. 2020, 5(8): https://www.webofscience.com/wos/woscc/full-record/WOS:000557740000007.
[18] Qi, Han, Li, Xinliang, Yu, Changping. Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows. ACTA MECHANICA SINICA[J]. 2020, 36(3): 692-700, http://lib.cqvip.com/Qikan/Article/Detail?id=7102558257.
[19] Xin Li, FuLin Tong, ChangPing Yu, XinLiang Li. Correlation between density and temperature fluctuations of hypersonic turbulent boundary layers at Ma∞ = 8. AIP Advances[J]. 2020, 10(7): https://doaj.org/article/159cb0855ca7431c9fd80b1736f0d90b.
[20] Tong, Fulin, Li, Xinliang, Yuan, Xianxu, Yu, Changping. Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner. COMPUTERS & FLUIDS[J]. 2020, 198: http://dx.doi.org/10.1016/j.compfluid.2019.104385.
[21] 党冠麟, 刘世伟, 胡晓东, 张鉴, 李新亮. 基于CPU/GPU异构系统架构的高超声速湍流直接数值模拟研究. 数据与计算发展前沿. 2020, 2(1): 105-116, http://lib.cqvip.com/Qikan/Article/Detail?id=7101588172.
[22] Li, Xin, Tong, FuLin, Yu, ChangPing, Li, XinLiang. Correlation between density and temperature fluctuations of hypersonic turbulent boundary layers at Ma(infinity)=8. AIP ADVANCES[J]. 2020, 10(7): https://www.webofscience.com/wos/woscc/full-record/WOS:000551864600001.
[23] 于长平, 李新亮, 闫政, 齐涵. 螺旋湍流的相关研究进展. 2020, 1-, https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CPFD&dbname=CPFDTEMPDAY&filename=AGLU202012001115&v=MjAzNTVIZTdHNEhOSE5yWTlGWmVvT0NSTkt1aGRobmo5OFRuanFxeGRFZU1PVUtyaWZaZWR2RnlubFVyL0pJbDRjSkNy.
[24] 童福林, 孙东, 袁先旭, 李新亮. 超声速膨胀角入射激波/湍流边界层干扰直接数值模拟. 航空学报[J]. 2020, 41(3): 134-153, http://lib.cqvip.com/Qikan/Article/Detail?id=7101781704.
[25] 李芳, 李志辉, 徐金秀, 范昊, 褚学森, 李新亮. 基于十亿亿次国产超算系统的流体力学软件众核适应性研究. 计算机科学[J]. 2020, 47(1): 24-30, http://lib.cqvip.com/Qikan/Article/Detail?id=7100754623.
[26] Li, Xin, Yu, ChangPing, Li, Li, Li, XinLiang. An improved weighted essentially non-oscillatory scheme with modified smoothness indicator tau and adaptive index p. INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS[J]. 2020, 34(4): 299-313, https://www.webofscience.com/wos/woscc/full-record/WOS:000531930100001.
[27] XiaoPing Chen, XinLiang Li, ZuChao Zhu. Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas. 中国科学:物理学、力学、天文学英文版[J]. 2019, 64-74, http://lib.cqvip.com/Qikan/Article/Detail?id=74718871504849574854484856.
[28] Fu, Yaowei, Yu, Changping, Yan, Zheng, Li, Xinliang. The Effects of Combustion on Turbulent Statistics in a Supersonic Turbulent Jet. ADVANCES IN APPLIED MATHEMATICS AND MECHANICS[J]. 2019, 11(3): 664-674, http://dspace.imech.ac.cn/handle/311007/78445.
[29] Li, Xin, Tong, FuLin, Yu, ChangPing, Li, XinLiang. Statistical analysis of temperature distribution on vortex surfaces in hypersonic turbulent boundary layer. PHYSICS OF FLUIDS[J]. 2019, 31(10): https://www.webofscience.com/wos/woscc/full-record/WOS:000506026700018.
[30] Yan, Zheng, Li, Xinliang, Wang, Jianchun, Yu, Changping. Effect of pressure on joint cascade of kinetic energy and helicity in compressible helical turbulence. PHYSICAL REVIEW E[J]. 2019, 99(3): http://dspace.imech.ac.cn/handle/311007/78925.
[31] Chen, XiaoPing, Li, XinLiang, Zhu, ZuChao. Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2019, 62(6): http://lib.cqvip.com/Qikan/Article/Detail?id=74718871504849574854484856.
[32] 李理, 刘晓艳, 李新亮, 田保林, 梁贤, 哈金才. 高精度格式非线性权的统计谱特性分析. 计算物理[J]. 2019, 127-140, http://lib.cqvip.com/Qikan/Article/Detail?id=74838776504849574850484849.
[33] 田奇, 郭元, 梁贤, 李新亮. 自适应的高精度中心-WENO混合格式. 空气动力学学报[J]. 2019, 37(4): 541-545,577, http://lib.cqvip.com/Qikan/Article/Detail?id=7100174949.
[34] Li Xinliang. Direct numerical simulation of wall temperature effects on the Reynold stress of flat-plate turbulent boundary layer. Advances in Applied Mathematics and Mechanics. 2019, [35] Zhou, Hao, Li, Xinliang, Qi, Han, Yu, Changping. Subgrid-scale model for large-eddy simulation of transition and turbulence in compressible flows. PHYSICS OF FLUIDS[J]. 2019, 31(12): https://www.webofscience.com/wos/woscc/full-record/WOS:000531265100001.
[36] Yan, Zheng, Li, Xinliang, Fu, Yaowei, Yu, Changping. The Effect of Helicity on Kinetic Energy Cascade in Compressible Helical Turbulence. ADVANCES IN APPLIED MATHEMATICS AND MECHANICS[J]. 2019, 11(3): 700-710, http://dspace.imech.ac.cn/handle/311007/78444.
[37] Li, Xin, Yu, Changping, Li, Xinliang. Wall Temperature Effects on the Reynold Stress of Flat-Plate Turbulent Boundary Layer: a Numerical Investigation. ADVANCES IN APPLIED MATHEMATICS AND MECHANICS[J]. 2019, 11(3): 653-663, http://dspace.imech.ac.cn/handle/311007/78447.
[38] Fu, Yaowei, Yu, Changping, Yan, Zheng, Li, Xinliang. DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2019, 93: http://dx.doi.org/10.1016/j.ast.2019.105362.
[39] Liu, Wanhai, Li, Xinliang, Yu, Changping, Fu, Yaowei, Wang, Pei, Wang, Lili, Ye, Wenhua. Theoretical study on finite-thickness effect on harmonics in Richtmyer-Meshkov instability for arbitrary Atwood numbers. PHYSICS OF PLASMAS[J]. 2018, 25(12): http://dspace.imech.ac.cn/handle/311007/78224.
[40] 李新亮, 于长平, 童福林. DNS of Turbulent Compression Ramp Flow with Mach 6. 7th European Conference on Computational Fluid Dynamics (ECFD 7)null. 2018, http://dspace.imech.ac.cn/handle/311007/78052.
[41] 李新亮, 于长平, 童福林. Direct Numerical Simulation of Hypersonic Boundary-layer Transition of Blunt cones. Tenth International Conference on Computational Fluid Dynamics (ICCFD10)null. 2018, http://dspace.imech.ac.cn/handle/311007/78051.
[42] 李新亮, 刘洪伟, 于长平. A hybrid kinetic weno scheme for compressible flow simulations. Proeedings of The Tenth International Conference on Computational Fluid Dynamicsnull. 2018, ICCFD10-2018, http://dspace.imech.ac.cn/handle/311007/78029.
[43] 李新亮, 童福林, 于长平, 李欣. 激波-湍流边界层干扰直接数值模拟研究. 首届中国空气动力学大会论文集null. 2018, http://dspace.imech.ac.cn/handle/311007/78054.
[44] Tong, Fulin, Yu, Changping, Tang, Zhigong, Li, Xinliang. Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects. COMPUTERS & FLUIDS[J]. 2017, 149: 56-69, http://dx.doi.org/10.1016/j.compfluid.2017.03.009.
[45] Tong, Fulin, Li, Xinliang, Duan, Yanhui, Yu, Changping. Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp. PHYSICS OF FLUIDS[J]. 2017, 29(12): http://dspace.imech.ac.cn/handle/311007/72162.
[46] Tong, Fulin, Tang, Zhigong, Yu, Changping, Zhu, Xingkun, Li, Xinliang. Numerical analysis of shock wave and supersonic turbulent boundary interaction between adiabatic and cold walls. JOURNAL OF TURBULENCE[J]. 2017, 18(6): 569-588, https://www.webofscience.com/wos/woscc/full-record/WOS:000400379700005.
[47] Yu, Changping, Xiao, Zuoli, Li, Xinliang. Scale-adaptive subgrid-scale modelling for large-eddy simulation of turbulent flows. PHYSICS OF FLUIDS[J]. 2017, 29(3): http://dspace.imech.ac.cn/handle/311007/60586.
[48] 童福林, 李新亮, 唐志共. 激波与转捩边界层干扰非定常特性数值分析. 力学学报[J]. 2017, 49(1): 93-104, http://dspace.imech.ac.cn/handle/311007/72014.
[49] Tong Fulin, Yu Changping, Tang Zhigong, Li Xinliang. Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects. Computers and Fluids[J]. 2017, 149: 56-69, http://dx.doi.org/10.1016/j.compfluid.2017.03.009.
[50] Liu, Wanhai, Yu, Changping, Jiang, Hongbin, Li, Xinliang. Bell-Plessett effect on harmonic evolution of spherical Rayleigh-Taylor instability in weakly nonlinear scheme for arbitrary Atwood numbers. PHYSICS OF PLASMAS[J]. 2017, 24(2): http://dspace.imech.ac.cn/handle/311007/60572.
[51] Zhu, XingKun, Yu, ChangPing, Tong, FuLin, Li, XinLiang. Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction. AIAA JOURNAL[J]. 2017, 55(1): 131-140, http://www.irgrid.ac.cn/handle/1471x/1179239.
[52] 童福林, 李新亮, 唐志共. 激波与转捩边界层干扰非定常特性数值分析1). 力学学报. 2017, 49(1): 93-104, http://lib.cqvip.com/Qikan/Article/Detail?id=7000105819.
[53] Zhang, Yousheng, He, Zhiwei, Gao, Fujie, Li, Xinliang, Tian, Baolin. Evolution of mixing width induced by general Rayleigh-Taylor instability. PHYSICAL REVIEW E[J]. 2016, 93(6): http://www.irgrid.ac.cn/handle/1471x/1093278.
[54] He, Zhiwei, Zhang, Yousheng, Li, Xinliang, Tian, Baolin. Preventing numerical oscillations in the flux-split based finite difference method for compressible flows with discontinuities, II. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS[J]. 2016, 80(5): 306-316, http://www.irgrid.ac.cn/handle/1471x/1035741.
[55] Li, Xuesong, Li, Xinliang. All-speed Roe scheme for the large eddy simulation of homogeneous decaying turbulence. INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS[J]. 2016, 30(1): 69-78, http://www.irgrid.ac.cn/handle/1471x/1093271.
[56] Li, Li, Yu, Changping, Chen, Zhe, Li, Xinliang. Resolution-optimised nonlinear scheme for secondary derivatives. INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS[J]. 2016, 30(2): 107-119, http://www.irgrid.ac.cn/handle/1471x/1103874.
[57] Chen, Zhe, Yu, ChangPing, Li, Li, Li, XinLiang. Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMYnull. 2016, 59(6): http://www.irgrid.ac.cn/handle/1471x/1093284.
[58] Wang, Bing, Hu, Xiangyu, Li, Xinliang, Wang, Qiang. Numerical study on super/hypersonic flow, mixing, and combustion phenomena, 2015. ADVANCES IN MECHANICAL ENGINEERINGnull. 2016, 8(2): http://www.irgrid.ac.cn/handle/1471x/1093269.
[59] 童福林, 李新亮, 唐志共, 朱兴坤, 黄江涛. 转捩对压缩拐角激波/边界层干扰分离泡的影响. 航空学报[J]. 2016, 37(10): 2909-2921, http://www.irgrid.ac.cn/handle/1471x/1121967.
[60] He, Zhiwei, Zhang, Yousheng, Gao, Fujie, Li, Xinliang, Tian, Baolin. An improved accurate monotonicity-preserving scheme for the Euler equations. COMPUTERS & FLUIDS[J]. 2016, 140: 1-10, http://dx.doi.org/10.1016/j.compfluid.2016.09.002.
[61] 童福林, 唐志共, 李新亮, 吴晓军, 朱兴坤. 压缩拐角激波与旁路转捩边界层干扰数值研究. 航空学报[J]. 2016, 37(12): 3588-3604, http://dspace.imech.ac.cn/handle/311007/72062.
[62] Zhiwei He, Yousheng Zhang, Fujie Gao, Xinliang Li, Baolin Tian. An improved accurate monotonicity-preserving scheme for the Euler equations. Computers and Fluids. 2016, 140: 1-10, http://dx.doi.org/10.1016/j.compfluid.2016.09.002.
[63] Yu, Changping, Xiao, Zuoli, Li, Xinliang. Dynamic optimization methodology based on subgrid-scale dissipation for large eddy simulation. PHYSICS OF FLUIDS[J]. 2016, 28(1): http://www.irgrid.ac.cn/handle/1471x/1093279.
[64] He, Zhiwei, Zhang, Yousheng, Li, Xinliang, Li, Li, Tian, Baolin. Preventing numerical oscillations in the flux-split based finite difference method for compressible flows with discontinuities. JOURNAL OF COMPUTATIONAL PHYSICS[J]. 2015, 300: 269-287, http://dx.doi.org/10.1016/j.jcp.2015.07.049.
[65] Liang, Xian, Li, Xinliang. Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer. COMMUNICATIONS IN COMPUTATIONAL PHYSICS[J]. 2015, 17(1): 189-212, http://www.irgrid.ac.cn/handle/1471x/949852.
[66] 张天文, 李新亮, 张鉴, 陆忠华. 高精度湍流直接数值模拟程序的异构并行优化分析. 科研信息化技术与应用[J]. 2015, 3-11, http://www.irgrid.ac.cn/handle/1471x/1093258.
[67] 李新亮. 高超声速湍流直接数值模拟技术. 航空学报[J]. 2015, 36(1): 147-158, http://www.irgrid.ac.cn/handle/1471x/1010576.
[68] 张又升, 田保林, 何志伟, 高福杰, 李新亮. 对称(破缺)观下控制瑞利-泰勒不稳定性后期混合宽度演化的守恒性原理. 中国力学大会-2015论文摘要集null. 2015, http://www.irgrid.ac.cn/handle/1471x/1093300.
[69] 朱兴坤, 于长平, 李新亮. 壁温对激波-湍流边界层干扰的影响规律研究. 第八届全国高超声速科技学术会议论文摘要集null. 2015, http://www.irgrid.ac.cn/handle/1471x/1093308.
[70] 李理, 陈哲, 何志伟, 李新亮. 非线性权在谱空间中的性质分析. 中国力学大会-2015论文摘要集null. 2015, http://www.irgrid.ac.cn/handle/1471x/1093296.
[71] 张又升, 何志伟, 李新亮, 田保林. The Realization of Non-reflecting Boundaries for Compressible Rayleigh-Taylor Flows with Variable Acceleration Histories. Procedia Engineering[J]. 2015, 126: 118-122, http://www.irgrid.ac.cn/handle/1471x/1093264.
[72] Liu, Wanhai, Chen, Yulian, Yu, Changping, Li, Xinliang. Harmonic growth of spherical Rayleigh-Taylor instability in weakly nonlinear regime. PHYSICS OF PLASMAS[J]. 2015, 22(11): http://www.irgrid.ac.cn/handle/1471x/1035746.
[73] 李新亮, 傅德薰, 马延文. 捕捉激波的群速度控制方法. 空气动力学学报. 2014, 32(5): 575-580, http://lib.cqvip.com/Qikan/Article/Detail?id=662842686.
[74] Zhao, Rui, Rong, Jili, Li, Xinliang. Entropy and its application in turbulence modeling. CHINESE SCIENCE BULLETIN[J]. 2014, 59(31): 4137-4141, http://www.irgrid.ac.cn/handle/1471x/1757576.
[75] 于长平, 李新亮. 基于螺旋度的亚格子模型的提出与推广. 第八届全国流体力学学术会议论文摘要集null. 2014, http://www.irgrid.ac.cn/handle/1471x/956424.
[76] 孙阳, 李新亮, 艾晓辉. Hermite WENO DG/FV混合算法的研究与应用. 第八届全国流体力学学术会议论文摘要集null. 2014, http://www.irgrid.ac.cn/handle/1471x/956434.
[77] He ZhiWei, Li XinLiang, Liang Xian. Nonlinear spectral-like schemes for hybrid schemes. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2014, 57(4): 753-763, http://www.irgrid.ac.cn/handle/1471x/837181.
[78] Wang, Bing, Hu, X Y, Li, Xinliang, Wang, Qiang. Numerical Study on Super/Hypersonic Flow, Mixing, and Combustion Phenomena. ADVANCES IN MECHANICAL ENGINEERINGnull. 2014, 6: http://www.irgrid.ac.cn/handle/1471x/845388.
[79] 张又升, 田包林, 何志伟, 李新亮. 基于特征波方法的可压缩瑞利-泰勒流动无反射边界条件. 第八届全国流体力学学术会议论文摘要集null. 2014, http://www.irgrid.ac.cn/handle/1471x/956436.
[80] 田保林, 张又升, 李新亮. 可压缩Rayleigh-Taylor不稳定性及湍流混合的直接数值模拟. 第八届全国流体力学学术会议论文摘要集null. 2014, http://www.irgrid.ac.cn/handle/1471x/956471.
[81] Liu, Wanhai, Yu, Changping, Li, Xinliang. Effects of initial radius of the interface and Atwood number on nonlinear saturation amplitudes in cylindrical Rayleigh-Taylor instability. PHYSICS OF PLASMAS[J]. 2014, 21(11): http://www.irgrid.ac.cn/handle/1471x/909766.
[82] 赵瑞, 阎超, 李新亮, 蒋海军. 比熵增概念及其在湍流模型中的应用. 空气动力学学报. 2013, 31(3): 381-387, http://lib.cqvip.com/Qikan/Article/Detail?id=46262248.
[83] 叶钦巴图, 胡晓东, 张鉴, 陆忠华, 李新亮. 并行WENO格式在三维定常粘性流体计算中的应用. 科研信息化技术与应用[J]. 2013, 4(5): 76-89, http://www.irgrid.ac.cn/handle/1471x/862701.
[84] Zhao Rui, Yan Chao, Yu Jian, Li Xinliang. Improvement of Baldwin-Lomax turbulence model for supersonic complex flows. CHINESE JOURNAL OF AERONAUTICS[J]. 2013, 26(3): 529-534, http://www.irgrid.ac.cn/handle/1471x/709254.
[85] Li, Xinliang, Leng, Yan, He, Zhiwei. Optimized sixth-order monotonicity-preserving scheme by nonlinear spectral analysis. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS[J]. 2013, 73(6): 560-577, http://www.irgrid.ac.cn/handle/1471x/709253.
[86] 李理, 陈哲, 李新亮. 离散NS 方程熵增分析. 高温气体动力学研究进展null. 2013, 159-164, http://www.irgrid.ac.cn/handle/1471x/811625.
[87] 李理, 李新亮. 保墒增的高阶人工黏性法. 中国力学大会——2013论文摘要集null. 2013, http://www.irgrid.ac.cn/handle/1471x/831896.
[88] 陈小平, 李新亮, 窦华书. 超声速燃烧室隔离段壁面热流的分析. 中国力学大会——2013论文摘要集null. 2013, http://www.irgrid.ac.cn/handle/1471x/831762.
[89] 陈哲, 李新亮, 李理. 流向肋条平板边界层湍流减阻研究. 中国力学大会——2013论文摘要集null. 2013, http://www.irgrid.ac.cn/handle/1471x/831747.
[90] 刘冰, 陆忠华, 李新亮, 胡晓东. 基于GPU的多重网格Navier-Stokes解算器并行优化方法研究. 科研信息化技术与应用:中英文. 2013, 4(3): 56-67, http://lib.cqvip.com/Qikan/Article/Detail?id=46714872.
[91] 陈小平, 李新亮, 仲峰泉. 参考焓值法在高速槽道湍流中的修正. 力学学报[J]. 2013, 45(4): 614-618, http://www.irgrid.ac.cn/handle/1471x/673250.
[92] 李新亮, 何志伟, 梁贤. 入射激波-湍流边界层干扰的直接数值模拟. 中国力学大会——2013论文摘要集null. 2013, http://www.irgrid.ac.cn/handle/1471x/831746.
[93] 吴斌, 邹鸿岳, 胡延超, 陈曦, 毕卫涛, 李新亮, 佘振苏. 超音速压缩拐角平均速度剖面的定量理论. 中国力学大会——2013论文摘要集null. 2013, http://www.irgrid.ac.cn/handle/1471x/831745.
[94] Liang Xian, Li XinLiang. DNS of a spatially evolving hypersonic turbulent boundary layer at Mach 8. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2013, 56(7): 1408-1418, http://www.irgrid.ac.cn/handle/1471x/648506.
[95] Zhao Rui, Yan Chao, Li XinLiang, Kong WeiXuan. Towards an entropy-based detached-eddy simulation. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2013, 56(10): 1970-1980, http://www.irgrid.ac.cn/handle/1471x/726399.
[96] 陈小平, 李新亮. Direct Numerical Simulation of Chemical Non-equilibrium Turbulent Flow. CHINESE PHYSICS LETTERS[J]. 2013, 30(6): 118-122, http://www.irgrid.ac.cn/handle/1471x/709252.
[97] 梁贤, 李新亮. 高超声速小钝度球锥边界层转捩的攻角效应的直接数值模拟. 中国力学大会——2013论文摘要集null. 2013, http://www.irgrid.ac.cn/handle/1471x/831765.
[98] Leng Yan, Li XinLiang, Fu DeXun, Ma YanWen. Optimization of the MUSCL scheme by dispersion and dissipation. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2012, 55(5): 844-853, http://lib.cqvip.com/Qikan/Article/Detail?id=41556479.
[99] 李理, 李新亮. 保证极值点精度的高阶保单调格式. 高温气体动力学研究进展null. 2012, 134-138, http://www.irgrid.ac.cn/handle/1471x/811574.
[100] LENG Yan, LI XinLiang, FU DeXun, MA YanWen. Optimization of the MUSCL scheme by dispersion and dissipation. 中国科学:物理学、力学、天文学英文版. 2012, 55(5): 844-853, http://lib.cqvip.com/Qikan/Article/Detail?id=41556479.
[101] 李新亮, 傅德薰, 马延文. 基于直接数值模拟的可压缩湍流模型评估和改进. 力学学报[J]. 2012, 44(2): 222-229, http://lib.cqvip.com/Qikan/Article/Detail?id=41251574.
[102] 梁贤, 李新亮. 超/高超声速边界层湍流的马赫数壁温效应. 高超声速专题研讨会暨第五届全国高超声速科学技术会议论文集null. 2012, 200-200, http://www.irgrid.ac.cn/handle/1471x/831696.
[103] 梁贤, 李新亮, 傅德薰, 马延文. Mach8的平板可压缩湍流边界层直接数值模拟及分析. 中国科学:物理学、力学、天文学. 2012, 42(3): 282-293, http://lib.cqvip.com/Qikan/Article/Detail?id=41093770.
[104] 李新亮, 傅德薰, 马延文. 基于直接数值模拟的可压缩湍流模型评估与改进. 力学学报[J]. 2012, 44(2): 222-229, http://www.irgrid.ac.cn/handle/1471x/516969.
[105] 何志伟, 李新亮. Mach23 的激波-平板湍流边界层干扰的直接数值模拟. 高温气体动力学研究进展null. 2012, 271-279, http://www.irgrid.ac.cn/handle/1471x/811597.
[106] 陈哲, 李新亮, 梁贤. 流向细纹平板边界层湍流减阻机理研究. 高温气体动力学研究进展null. 2012, 265-270, http://www.irgrid.ac.cn/handle/1471x/811596.
[107] Zhang, YouSheng, Bi, WeiTao, Hussain, Fazle, Li, XinLiang, She, ZhenSu. Mach-Number-Invariant Mean-Velocity Profile of Compressible Turbulent Boundary Layers. PHYSICAL REVIEW LETTERS[J]. 2012, 109(5): http://www.irgrid.ac.cn/handle/1471x/516968.
[108] 李新亮, 冷岩. 非线性优化的保单调差分格式. 高温气体动力学研究进展null. 2012, 139-143, http://www.irgrid.ac.cn/handle/1471x/811575.
[109] 梁贤, 李新亮, 王子梁. 超/高超声速平板湍流边界层的 DNS 和特征分析. 高温气体动力学研究进展null. 2012, 289-296, http://www.irgrid.ac.cn/handle/1471x/811600.
[110] 梁贤, 李新亮, 傅德薰, 马延文. 万核级可扩展CFD软件及应用. 华中科技大学学报(自然科学版)[J]. 2011, 39(S1): 67-70, http://www.irgrid.ac.cn/handle/1471x/390265.
[111] 李新亮, 傅德薰, 马延文, 梁贤. DNS of shock/boundary layer interaction flow in a supersonic compression ramp. COMPUTATIONAL FLUID DYNAMICS 2010null. 2011, 729-737, http://www.irgrid.ac.cn/handle/1471x/586039.
[112] HE ZhiWei, LI XinLiang, FU DeXun, MA YanWen. A 5th order monotonicity-preserving upwind compact difference scheme. 中国科学:物理学、力学、天文学英文版. 2011, 54(3): 511-522, http://lib.cqvip.com/Qikan/Article/Detail?id=36943841.
[113] 陈小平, 李新亮. 高温气体效应对高超声速槽道湍流边界层的影响. 高温气体动力学研究进展null. 2011, 54-59, http://www.irgrid.ac.cn/handle/1471x/811501.
[114] 李新亮, 冷岩, 何志伟. 优化的保单调差分格式及激波/湍流边界层干扰的直接数值模拟. 第四届高超声速科技学术会议会议日程及摘要集null. 2011, 10-, http://www.irgrid.ac.cn/handle/1471x/390287.
[115] 董廷星, 李新亮, 李森, 迟学斌. GPU上计算流体力学的加速. 计算机系统应用. 2011, 104-109, http://lib.cqvip.com/Qikan/Article/Detail?id=36254961.
[116] 陈小平, 李新亮, 樊菁. 高超声速高温槽道湍流摩阻/热流分析. 第四届高超声速科技学术会议会议日程及摘要集null. 2011, 20-, http://www.irgrid.ac.cn/handle/1471x/390276.
[117] 李森, 李新亮, 王龙, 陆忠华, 迟学斌. 基于OpenCL的并行方腔流加速性能分析. 计算机应用研究. 2011, 28(4): 1401-1403, http://lib.cqvip.com/Qikan/Article/Detail?id=37266432.
[118] He ZhiWei, Li XinLiang, Fu DeXun, Ma YanWen. A 5th order monotonicity-preserving upwind compact difference scheme. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2011, 54(3): 511-522, http://lib.cqvip.com/Qikan/Article/Detail?id=36943841.
[119] 陈小平, 李新亮, 樊菁. 变比热真实气体效应的高超声速槽道湍流直接数值模拟. 中国科学:物理学、力学、天文学. 2011, 41(8): 969-979, http://lib.cqvip.com/Qikan/Article/Detail?id=38771537.
[120] Dong Ming, Li XinLiang. Problems of the conventional BL model as applied to super/hypersonic turbulent boundary layers and its improvements. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2011, 54(10): 1889-1898, http://dx.doi.org/10.1007/s11433-011-4450-6.
[121] 梁贤, 李新亮, 傅德薰, 马延文. 壁温影响的高超声速湍流边界层特征. 第四届高超声速科技学术会议会议日程及摘要集null. 2011, 9-, http://www.irgrid.ac.cn/handle/1471x/390288.
[122] DONG Ming, LI XinLiang. Problems of the conventional BL model as applied to super/hypersonic turbulent boundary layers and its improvements. 中国科学:物理学、力学、天文学英文版. 2011, 54(10): 1889-1898, http://lib.cqvip.com/Qikan/Article/Detail?id=39210565.
[123] 何志伟, 李新亮, 傅德薰, 马延文. 求解双曲型守恒律的修正加权群速度控制格式. 高温气体动力学研究进展null. 2011, 133-144, http://www.irgrid.ac.cn/handle/1471x/811515.
[124] 梁贤, 李新亮, 傅德薰, 马延文. Mach8 的平板可压缩湍流边界层直接数值模拟. 高温气体动力学研究进展null. 2011, 220-229, http://www.irgrid.ac.cn/handle/1471x/811527.
[125] 冷岩, 李新亮, 傅德薰, 马延文. Optimization of MUSCL scheme by dispersion and dissipation. 高温气体动力学研究进展null. 2011, 145-156, http://www.irgrid.ac.cn/handle/1471x/811516.
[126] 李新亮, 何志伟, 冷岩. 飞行器复杂流动高精度数值方法研究. 高温气体动力学研究进展null. 2011, 113-119, http://www.irgrid.ac.cn/handle/1471x/811512.
[127] 傅德薰, 李新亮, 马延文. 可压缩湍流直接数值模拟. 北京:科学出版社.2010[M]. 2010, http://dspace.imech.ac.cn/handle/311007/43241.
[128] 李新亮, 傅德薰, 马延文, 梁贤. 压缩折角激波-湍流边界层干扰直接数值模拟. 中国科学:物理学、力学、天文学. 2010, 791-799, http://lib.cqvip.com/Qikan/Article/Detail?id=34256227.
[129] Li, XinLiang, Fu, DeXun, Ma, YanWen, Liang, Xian. Direct numerical simulation of compressible turbulent flows. ACTA MECHANICA SINICAnull. 2010, 26(6): 795-806, http://lib.cqvip.com/Qikan/Article/Detail?id=37261170.
[130] 傅德薰, 马延文, 李新亮. 基于直接数值模拟的超/高超声速湍流模型评估与改进. 第三届高超声速科技学术会议.江苏·无锡.2010年10月26-28日null. 2010, http://dspace.imech.ac.cn/handle/311007/44211.
[131] Li XinLiang, Fu DeXun, Ma YanWen, Liang Xian. Direct numerical simulation of shock/turbulent boundary layer interaction in a supersonic compression ramp. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY[J]. 2010, 53(9): 1651-1658, http://dspace.imech.ac.cn/handle/311007/42444.
[132] Li, Xinliang, Fu, Dexun, Ma, Yanwen. Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack. PHYSICS OF FLUIDS[J]. 2010, 22(2): http://dspace.imech.ac.cn/handle/311007/33062.
[133] Liang, Xian, Li, Xinliang, Fu, Dexun, Ma, Yanwen. Effects of wall temperature on boundary layer stability over a blunt cone at Mach 7.99. COMPUTERS & FLUIDS[J]. 2010, 39(2): 359-371, http://dx.doi.org/10.1016/j.compfluid.2009.09.015.
[134] Ma YW, 李新亮, 马延文, 傅德薰. A New High Order Accurate Shock Capture Method with Wave Booster. ISCM II AND EPMESC XII, PTS 1 AND 2null. 2010, 1363-1367, http://dspace.imech.ac.cn/handle/311007/44316.
[135] 李新亮, 傅德薰, 马延文, 高慧. Acoustic Calculation for Supersonic Turbulent Boundary Layer Flow. 中国物理快报:英文版. 2009, 26(9): 181-184, http://lib.cqvip.com/Qikan/Article/Detail?id=31479116.
[136] Liang, Xian, Li, Xinliang, Fu, Dexun, Ma, Yanwen. Complex Transition of Double-Diffusive Convection in a Rectangular Enclosure with Height-to-Length Ratio Equal to 4: Part I. COMMUNICATIONS IN COMPUTATIONAL PHYSICS[J]. 2009, 6(2): 247-268, http://dspace.imech.ac.cn/handle/311007/28799.
[137] Li XinLiang, Fu DeXun, Ma YanWen, Gao Hui. Acoustic Calculation for Supersonic Turbulent Boundary Layer Flow. CHINESE PHYSICS LETTERS[J]. 2009, 26(9): http://lib.cqvip.com/Qikan/Article/Detail?id=31479116.
[138] Zhang YuDong, Fu DeXun, Ma YanWen, Li XinLiang. Receptivity to free-stream disturbance waves for hypersonic flow over a blunt cone. SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY[J]. 2008, 51(11): 1682-1690, http://dspace.imech.ac.cn/handle/311007/25880.
[139] 李新亮, 傅德薰, 马延文. 可压缩尖锥边界层湍流的直接数值模拟. 中国科学. G辑, 物理学,力学,天文学[J]. 2008, 38(1): 89-101, http://lib.cqvip.com/Qikan/Article/Detail?id=29070195.
[140] 李新亮, 傅德薰, 马延文. 可压缩尖锥边界层湍流的直接数值模拟. 中国科学:G辑. 2008, 38(1): 89-101, http://lib.cqvip.com/Qikan/Article/Detail?id=29070195.
[141] Fu DeXun, Ma YanWen, Li XinLiang. Direct numerical simulation of three-dimensional Richtmyer-Meshkov instability. CHINESE PHYSICS LETTERS[J]. 2008, 25(1): 188-190, http://lib.cqvip.com/Qikan/Article/Detail?id=26464133.
[142] Zhang YuDong, Fu DeXun, Ma YanWen, Li XinLiang. Receptivity to free-stream disturbance waves for hypersonic flow over a blunt cone. SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY[J]. 2008, 51(11): 1682-1690, http://dspace.imech.ac.cn/handle/311007/25880.
[143] 张玉东, 傅德薰, 马延文, 李新亮. 钝锥高超声速边界层来流感受性数值研究. 中国科学:G辑. 2008, 38(9): 1246-1254, http://lib.cqvip.com/Qikan/Article/Detail?id=29047300.
[144] 马延文, 傅德薰, 梁贤, 李新亮. 壁温对高超音速钝锥边界层稳定性的影响. 第五届全国青年计算物理学术交流会论文摘要.中国核学会,2008,p.83-84null. 2008, 83-84, http://dspace.imech.ac.cn/handle/311007/34392.
[145] 张玉东, 傅德薰, 马延文, 李新亮. 钝锥高超声速边界层来流感受性数值研究. 中国科学. G辑, 物理学,力学,天文学[J]. 2008, 38(9): 1246-1254, http://lib.cqvip.com/Qikan/Article/Detail?id=29047300.
[146] Li, Xinliang, Fu, Dexun, Ma, Yanwen. Direct Numerical Simulation of Hypersonic Boundary-Layer Transition over a Blunt Cone. AIAA JOURNAL[J]. 2008, 46(11): 2899-2913, http://dspace.imech.ac.cn/handle/311007/25846.
[147] Li XinLiang, Fu DeXun, Ma YanWen. DNS of compressible turbulent boundary layer around a sharp cone. SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY[J]. 2008, 51(6): 699-714, http://dspace.imech.ac.cn/handle/311007/26034.
[148] Li, Xinliang, Hashimoto, Katsumi, Tominaga, Yasuhiro, Tanahashi, Mamoru, Miyauchi, Toshio. Numerical Study of Heat Transfer Mechanism in Turbulent Supercritical CO2 Channel Flow. JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY[J]. 2008, 3(1): 112-123, http://dspace.imech.ac.cn/handle/311007/25542.
[149] Li XinLiang, Fu DeXun, Ma YanWen. DNS of compressible turbulent boundary layer around a sharp cone. SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY[J]. 2008, 51(6): 699-714, http://dspace.imech.ac.cn/handle/311007/26034.
[150] Wang Yiting, Li Xinliang, Zhang Wuming, Zhang Liqiang. Building extraction of urban area from high resolution remotely sensed panchromatic data of urban area. Geoinformatics 2008 and Joint Conference on GIS and Built Environment: The Built Environment and Its Dynamicsnull. 2008, http://ir.ceode.ac.cn/handle/183411/30957.
[151] 贾效成, 李新亮, 丹阳, 路国辉, 王英强. 广东地区外来种五爪金龙的传粉生物学研究. 生物多样性[J]. 2007, 15(6): 592-598, http://ir.scbg.ac.cn/handle/344003/12601.
[152] 张玉东, 傅德薰, 马延文, 李新亮. 高精度非定常激波装配法. 计算物理. 2007, 24(5): 533-536, http://lib.cqvip.com/Qikan/Article/Detail?id=25376861.
[153] Zhou Ying, Li XinLiang, Fu DeXun, Ma YanWen. Coherent structures in transition of a flat-plate boundary layer at Ma=0.7. CHINESE PHYSICS LETTERS[J]. 2007, 24(1): 147-150, http://lib.cqvip.com/Qikan/Article/Detail?id=25742358.
[154] Zhang YD, 傅德薰, 马延文, 李新亮. Receptivity to free-stream disturbance waves for blunt cone axial symmetry hypersonic boundary layer. New Trends In Fluid Mechanics Research - Proceedings Of The Fifth International Conference On Fluid Mechanicsnull. 2007, 206-209, http://dspace.imech.ac.cn/handle/311007/25454.
[155] 周莹, 李新亮, 傅德薰, 马延文. Coherent Structures in Transition of a Flat-Plate Boundary Layer at Ma = 0.7. 中国物理快报:英文版. 2007, 24(1): 147-150, http://lib.cqvip.com/Qikan/Article/Detail?id=25742358.
[156] Li Xinliang, Fu Dexun, Groth C, Zingg DW. DNS of compressible turbulent boundary layer over a blunt wedge. COMPUTATIONAL FLUID DYNAMICS 2004, PROCEEDINGSnull. 2006, 555-+, http://apps.webofknowledge.com/CitedFullRecord.do?product=UA&colName=WOS&SID=5CCFccWmJJRAuMzNPjj&search_mode=CitedFullRecord&isickref=WOS:000240583500079.
[157] Li XinLiang, Fu DeXun, Ma YanWen. Direct numerical simulation of a spatially evolving supersonic turbulent boundary layer at Ma=6. CHINESE PHYSICS LETTERS[J]. 2006, 23(6): 1519-1522, http://dspace.imech.ac.cn/handle/311007/15846.
[158] 田保林, 傅德薰, 马延文, 李新亮. 迎风紧致格式求解Hamilton-Jacobi方程. 计算物理. 2005, 22(2): 117-122, http://lib.cqvip.com/Qikan/Article/Detail?id=15706868.
[159] 李新亮, 傅德薰, 马延文. Direct numerical simulation of round supersonic free jet. RECENT ADVANCES IN FLUID MECHANICSnull. 2004, http://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:000225709300159&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=3a85505900f77cc629623c3f2907beab.
[160] 李新亮, 傅德薰, 马延文. 可压缩钝楔边界层转捩到湍流的直接数值模拟. 中国科学:G辑[J]. 2004, 34(4): 466-480, http://lib.cqvip.com/Qikan/Article/Detail?id=10315907.
[161] 李新亮, 傅德薰, 马延文. 可压缩钝楔边界层转捩到湍流的直接数值模拟. 中国科学:G辑. 2004, 34(4): 466-480, http://lib.cqvip.com/Qikan/Article/Detail?id=10315907.
[162] 李新亮, 傅德薰, 马延文. 8阶群速度控制格式及其应用. 力学学报. 2004, 36(1): 79-83, http://lib.cqvip.com/Qikan/Article/Detail?id=9081122.
[163] 李新亮, 傅德薰, 马延文. 可压缩钝楔边界层转捩到湍流的直接数值模拟. 中国科学. G辑, 物理[J]. 2004, 34(4): 466-480, http://lib.cqvip.com/Qikan/Article/Detail?id=10315907.
[164] 李新亮, 傅德薰, 马延文. 可压衰减湍流中被动标量场的直接数值模拟及谱分析. 中国科学:G辑. 2003, 33(4): 357-367, http://lib.cqvip.com/Qikan/Article/Detail?id=8256123.
[165] 李新亮, 傅德薰, 马延文. 可压衰减湍流中被动标量场的直接数值模拟及谱分析. 中国科学. G辑, 物理[J]. 2003, 33(4): 357-367, http://lib.cqvip.com/Qikan/Article/Detail?id=8256123.
[166] 张志斌, 李新亮, 沈孟育. 三维直叶栅非定常流动的并行计算研究. 航空动力学报. 2003, 18(2): 283-288, http://lib.cqvip.com/Qikan/Article/Detail?id=7712094.
[167] 李新亮, 傅德薰, 马延文. 可压衰减湍流中被动标量场的直接数值模拟及谱分析. 中国科学:G辑[J]. 2003, 33(4): 357-367, http://lib.cqvip.com/Qikan/Article/Detail?id=8256123.
[168] 张志斌, 李新亮, 沈孟育. 平面压气机叶栅非定常流动的数值研究. 清华大学学报:自然科学版[J]. 2003, 43(2): 222-226, http://lib.cqvip.com/Qikan/Article/Detail?id=7446709.
[169] Li, XL, Fu, DX, Ma, YW. Direct numerical simulation of compressible isotropic turbulence. SCIENCE IN CHINA SERIES A-MATHEMATICS[J]. 2002, 45(11): 1452-1460, http://dspace.imech.ac.cn/handle/311007/15544.
[170] 李新亮, 马延文, 傅德薰. 迎风紧致格式的混淆误差分析及其同谱方法的比较. 计算物理. 2002, 19(4): 283-289, http://lib.cqvip.com/Qikan/Article/Detail?id=6552882.
[171] 李新亮, 傅德薰, 马延文. 可压缩衰减湍流的直接数值模拟. 计算流体力学研究进展——第十一届全国计算流体力学会议论文集null. 2002, 123-128, http://www.irgrid.ac.cn/handle/1471x/813625.
[172] 李新亮, 傅德薰. 可压缩均匀各向同性湍流的直接数值模拟. 中国科学:A辑. 2002, 32(8): 716-724, http://lib.cqvip.com/Qikan/Article/Detail?id=6649707.
[173] 李新亮, 傅德薰, 马延文. 可压缩均匀各向同性湍流的直接数值模拟. 中国科学. A辑, 数学[J]. 2002, 32(8): 716-724, http://lib.cqvip.com/Qikan/Article/Detail?id=6649707.
[174] 李新亮, 马延文, 傅德薰. 二维槽道湍流的标度律分析. 力学学报. 2002, 34(4): 604-608, http://lib.cqvip.com/Qikan/Article/Detail?id=6591541.
[175] 李新亮, 马延文, 傅德薰. 不可压N—S方程高效算法及二维槽道湍流分析. 力学学报. 2001, 33(5): 577-587, http://lib.cqvip.com/Qikan/Article/Detail?id=5595744.
[176] 李新亮, 马延文, 傅德薰. 可压槽道湍流的直接数值模拟及标度律分析. 中国科学. A辑, 数学[J]. 2001, 31(2): 153-, http://lib.cqvip.com/Qikan/Article/Detail?id=4997392.
[177] 傅德薰, 马延文, 李新亮, 王强. 剪切湍流的数值模拟及可压缩效应. 自然、工业与流动——第六届全国流体力学学术会议论文集null. 2001, 99-103, http://www.irgrid.ac.cn/handle/1471x/813601.
[178] 李新亮, 马延文. 可压槽道湍流的直接数值模拟及标度律分析. 中国科学:A辑. 2001, 31(2): 153-164, http://lib.cqvip.com/Qikan/Article/Detail?id=4997392.
[179] 李新亮. 槽道湍流的直接数值模拟. 博士论文.北京.中国科学院力学研究所,2000[D]. 2000, http://dspace.imech.ac.cn/handle/311007/23354.
[180] 李新亮. 槽道湍流的直接数值模拟. 博士论文.北京.中国科学院力学研究所,2000[D]. 2000, http://dspace.imech.ac.cn/handle/311007/23354.

指导学生

已指导学生

周莹  硕士研究生  080103-流体力学  

冷岩  硕士研究生  080103-流体力学  

何志伟  博士研究生  080103-流体力学  

陈小平  博士研究生  080103-流体力学  

现指导学生

康健  硕士研究生  080103-流体力学  

朱兴坤  硕士研究生  080103-流体力学  

李理  博士研究生  080103-流体力学  

陈哲  博士研究生  080103-流体力学  

周浩  硕士研究生  080104-工程力学  

王子梁  硕士研究生  080103-流体力学