李新亮

1990.08 ～ 1994.07 吉林大學數學系, 學士，應用力學

1994.08 ～ 1997.07 吉林大學數學研究所, 碩士, 流體力學

1997.08 ～ 2000.07 中國科學院力學研究所，博士 , 流體力學

2000.08 ～ 2002.07 清華大學工程力學系, 博士后, 流體力學

2002.08 ～至今 中國科學院力學研究所, 工作，流體力學

2005.08 ～ 2007.08 日本東京工業大學, JSPS特別研究員

2009.08 研究員

2011.07 博士生導師

計算流體力學；可壓縮湍流與轉捩；飛行器空氣動力學等

中國空氣動力學會物理氣體動力學專業委員會 副主任委員；計算物理學會常務理事；中國空氣動力學會計算流體力學專業委員會委員；力學學會計算流體力學專業組組員；北京大學湍流與複雜系統研究國家重點實驗室客座教授；《計算物理》編委；《中國物理快報》特邀評審；

1． Xinliang LI, Yanwen MA, Dexun Fu. 2000, DNS of Incompressible turbulent channel flow with upwind scheme on non-uniform meshes. Computational Fluid Dynamics JOURNAL

2． Li Xinliang, Ma Yanwen, Fu Dexun. DNS and scaling law analysis of compressible turbulent channel flow. Science in China另見: 李新亮，馬延文，傅德薰。可壓縮槽道湍流的直接數值模擬及標度律分析。中國科學

3． 李新亮，馬延文，傅德薰。不可壓N-S方程數值模擬方法研究及二維槽道流動的非線性行為分析。力學學報

4． 李新亮，馬延文，傅德薰。迎風緊緻格式的混淆誤差分析及其同譜方法的比較。計算物理

5． 李新亮，馬延文，傅德薰。二維可壓縮槽道湍流的標度律分析。力學學報

6． Li Xinliang, Fu Dexun, Ma Yanwen. Direct numerical simulation of compressible isotropic turbulence. Science in China 另見: 李新亮，傅德薰，馬延文。可壓縮均勻各向同性湍流的直接數值模擬。中國科學

7． 張志斌，李新亮，沈孟育。平面壓氣機葉柵非定常流動的數值模擬研究, 清華大學學報,(自然科學版),

8． 張志斌，李新亮，沈孟育。三維壓氣機直葉柵非定常流動的數值模擬研究, 航空動力學報

9． Fu Dexun, Ma Yanwen, Li Xinliang, and Liu Mingyu, Compact difference approximation with consistent boundary condition, Progress in Natural Science

10．Li Xinliang, Fu Dexun, Ma Yanwen. Direct numerical simulation of passive scalar in decaying compressible turbulence, Science in China 另見：李新亮 傅德薰 馬延文。可壓衰減湍流中被動標量場的直接數值模擬及譜分析，中國科學

11．李新亮，傅德薰，馬延文。八階群速度控制格式及其應用。力學學報

12．Linbo Zhang, Shiyi Chen, Xinliang Li et al. Some Numerical Results on the Domestic Made Teracluster LSSC—II. SCIENCE IN CHINA SERIES A-MATHEMATICS

13．Ma Yanwen, Gao Hui, Fu Dexun and Li Xinliang, Difference Scheme on Non-Uniform Mesh and Their Application, Progress in Natural Science,

14．Li Xinliang, Fu Dexun, and Ma Yanwen. DNS of compressible turbulent boundary layer over a blunt wedge. Science in China Ser.另見: 李新亮，傅德薰，馬延文。可壓縮鈍楔邊界層轉捩到湍流的直接數值模擬。中國科學

15．Xinliang Li, Dexun Fu, and Yanwen Ma. Optimized group velocity control scheme and DNS of decaying compressible turbulence of relative high turbulent Mach number. International Journal for Numerical Methods in Fluids,

16．Gao Hui, Fu Dexun, Ma Yanwen, Li Xinliang, Direct numerical simulation of supersonic boundary layer, Chinese Physics Letters

17．Li Xinliang, Fu Dexun and Ma Yanwen, Direct Numerical Simulation of a Spatially Evolving Supersonic Turbulent Boundary Layer at Ma = 6, Chinese Phys. Lett.

18．ZHOU Ying, LI Xin-Liang, FU De-Xun, MA Yan-Wen Coherent structures in the transition of a flat-plate boundary layer at Ma=0.7， Chinese Physics Letters

19． 張玉東，傅德薰，馬延文，李新亮。高精度非定常激波裝配法。計算物理

20． Fu Dexun, Ma Yanwen, Li Xinliang, Direct numerical simulation of three-dimensional Richtmyer-Mechkov instability, Chinese Physics Letters,

21．Li Xinliang, Fu Dexun and Ma Yanwen. DNS of compressible turbulent boundary layer around a sharp cone , Science in China另見：李新亮，傅德薰，馬延文。可壓縮尖錐邊界層轉捩的直接數值模擬，中國科學

22．Xinliang Li, Katsumi Hashimoto, Yasuhiro Tominaga, Mamoru Tanahashi and Toshio Miyauchi. Numerical study of heat transfer mechanism in turbulent supercritical CO2 channel flow. Journal of Thermal Science and Technology

23．Xinliang Li, Dexun Fu and Yanwen Ma，Direct numerical simulation of hypersonic boundary-layer transition over a blunt cone， AIAA Journal,

24． Zhang YD, Fu DX, Ma YW and Li XL, Receptivity to free-stream disturbance waves for hypersonic flow over a blunt cone, Science in China G另見：張玉東，傅德薰，馬延文，李新亮。鈍錐高超聲速邊界層來流感受性數值研究。中國科學

25．Xian Liang, Xinliang Li, Dexun Fu and Yanwen Ma, Complex Transition of Double –Diffusive Convection in a Rectangular Enclosure with Height-to-Length Ratio Equal to 4: Part I, COMMUNICATIONS IN COMPUTATIONAL PHYSICS

26．LI Xin-Liang, FU De-Xun, MA Yan-Wen and GAO Hui, Acoustic Calculation for Supersonic Turbulent Boundary Layer Flow, CHIN. PHYS. LETT

27．Xian Liang , Xinliang Li , Dexun Fu and Yanwen Ma, Effect of wall temperature on boundary layer stability over a blunt cone at Mach 7.99, Computers & Fluids

28．Xinliang Li, Dexun Fu and Yanwen Ma, Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack, Physics of Fluids

29．Xinliang Li, Dexun Fu，Yanwen Ma, Xian Liang, Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp， Science China： Physics, Mechanics & Astronomy, 另見：李新亮，傅德薰，馬延文，梁賢，壓縮折角激波-湍流邊界層干擾直接數值模擬，中國科學

30. Xinliang Li, Dexun Fu, Yanwen Ma and Xian Liang, Direct numerical simulation of compressible turbulent flows. Acta Mechanica Sinica

31. Zhiwei He, Xinliang Li, Dexun Fu and Yanwen Ma, Monotonicity-preserving Upwind Compact Difference Schemes, Science in China G, (已錄用，待發表)

32. 傅德薰，馬延文，李新亮，王強：可壓縮湍流直接數值模擬，科學出版社 (專著）