山西武术产生过“世界武术王子”原文庆和袁新东两代代表人物,袁晓超的出现标志着山西武术的第三代优秀人才正在崛起,逐渐走向成熟袁新东。

2003年10月,在亚洲武术青年锦标赛上获得两枚金牌。

2004年9月,在全国武术套路冠军赛中获得长拳冠军。

2005年十运会获得男子刀棍全能冠军。

2005年武术世界锦标赛男子长拳冠军。

国际期刊1. Xin Yuan, Accurate Simulations of Three-Dimensional Turbulent Flows with a Higher-Order High Resolution Scheme, CFD Journal, 1999, Vol. 8, No. 2, pp. 326-340.2. Xin Yuan, H. Daiguji, A Specially Combined Lower-Upper Factored Implicit Scheme For Three-Dimensional Compressible Navier-Stokes Equations, Computers and Fluids, 2001, Vol. 30, No. 3, pp. 339-363. SCI: 415MZ; EI: . Yan Jin, Xin Yuan, Numerical Study of Unsteady Viscous Flow Past Oscillating Airfoil, Wind Engineering, 2001, Vol. 25, No. 4, pp. 227-236. EI: RN 5522564. Shijie Zhang, Xin Yuan, and Dajun Ye, Analysis of Turbulent Separated Flows for the NREL Airfoil Using Anisotropic Two-Equation Models at Higher Angles of Attack, Wind Engineering, 2001, Vol. 25, No. 1, pp.41-53.5. Xin Yuan, Wind turbine research at Tsinghua University, China, Wind Engineering, 2001, Vol. 25, No. 1, pp. 65-66. (应邀在该杂志刊登本研究组的工作介绍与照片)国际会议6. Gang Xu, Xin Yuan, Dajun Ye, Development of a Higher-Order High Resolution Scheme for Three-Dimensional Turbulent Flow in Turbomachinery, in Proceedings: Fourth International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Dresden, Germany, 1999, Vol. II, pp. 305-310. ISTP: BR26G7. Gang Xu, Xin Yuan, Dajun Ye, Use of Neural Network Based Loss and Deviation Model in Flow Field Diagnosis of Multistage Axial Compressors, in Proceedings: 1st Int. Conf. on Engineering Thermophysics, Beijing, 1999, pp. 330-336.8. Jiangang Cai, Xin Yuan, Dajun Ye, A Preconditioning-Like Implicit Method for Low Speed Mixing Turbulent Flows, in Proceedings: 2nd Int. Symp. on Fluid Machinery and Fluid Engineering, 2000, pp. 73-80.9. Yan Jin, Xin Yuan, Numerical Study of Unsteady Viscous Flow Past Oscillating Airfoil, in Proceedings: 2nd Int. Symp. on Fluid Machinery and Fluid Engineering, 2000, pp. 404-409.10. Yuyang Lai, Xin Yuan. Blade Design Optimization With Three-Dimensional Viscous Analyses and Hybrid Optimization Approach, 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, USA Sept 4-6, 2002.AIAA No.: AIAA-2002-565811. Y. Jin, and X. Yuan, Numerical Analysis of the Airfoil’s Fluid-Structure Interaction Problems at Large Mean Incidence Angle, 2nd International Conference on Computational Fluid Dynamics, 2002, Sidney.12. Lin Zhirong and Yuan Xin, Multi-block Grid with Overlapping for Implicit Parallel Computation of Flow Field within Turbomachinery, 2nd International Conference on Computational Fluid Dynamics, 2002, Sidney.国内核心期刊13. 徐纲,袁新,叶大均,神经网络的非设计点损失落后角模型在流场诊断中的应用,工程热物理学报,1999, Vol. 20, No. 1, pp. 49-52.14. 袁新,江学忠,翼型大攻角低速分离流动的数值模拟,工程热物理学报,1999, Vol. 20, No. 2, pp. 161-165. EI: RN 214412915. 张宏武,徐纲,袁新,叶大均,应用高分辨率迎风格式精确分析透平叶栅三维湍流流场,工程热物理学报,1999, Vol. 20, No. 5, pp. 553-557. EI: . 蔡剑钢,袁新,叶大均,多组份混合工质掺混机理数值研究,工程热物理学报,2000, Vol. 21, No. 5, pp. 563-566. EI: . 张士杰,袁新,叶大均,跨音速轴流风扇转子流场三维粘性数值分析,推进技术,2000, Vol. 21, No. 6, pp. 40-43. EI: . 张士杰,袁新,叶大均,组合的LU分解迎风方法的多重网格收敛,清华大学学报(自然科学版),2000, Vol. 40, No. 2, pp. 90-93. EI: . 袁新,金琰,用高精度迎风格式模拟潜入式喷管流场,清华大学学报(自然科学版),2000, Vol. 40, No. 6, pp. 45-48. EI: . 张宏武,袁新,叶大均,透平叶栅大攻角流动特性的三维数值模拟,清华大学学报(自然科学版),2000, Vol. 40, No. 10, pp. 92-95. EI: . 张士杰,袁新,叶大均,全三维粘性流场计算的快速收敛方法,清华大学学报(自然科学版),2000, Vol. 40, No. 10, pp. 96-99. EI: . 蔡剑钢,袁新,叶大均,多组份混合工质掺混流动研究与工程应用,清华大学学报(自然科学版),2000, Vol. 40, No. 11, pp.43-46. EI: . 张宏武,江学忠,袁新,叶大均,二维翼型襟翼增升的数值模拟,清华大学学报(自然科学版),2000, Vol. 40, No. 11, pp. 55-58. EI: . Lidong He, Xin Yuan, Yan Jin, Zhenyou Zhu, Experimental Investigation of the Sealing Performance of Honeycomb Seals, Chinese Journal of Aeronautics, 2001, Vol. 14, No. 1, pp. 13-17. EI: RN 286718025. 徐纲,袁新,叶大均,采用高分辨率高精度格式求解跨音压气机转子内三维粘性流场,工程热物理学报,2001, Vol. 22, No. 1, pp. 44-47.26. 张宏武,袁新,叶大均,透平级非设计工况气动性能的数值模拟,工程热物理学报,2001, Vol. 22, No. 2, pp. 175-178.27. 蔡剑钢,袁新,叶大均,低速多组份混合工质掺混流场数值模拟的加速收敛,工程热物理学报,2001, Vol. 22, No. 3, pp. 298-300.28. 张士杰,袁新,叶大均,低展弦比跨音速轴流风扇转子流场三维数值模拟,工程热物理学报,2001, Vol. 22, No. 5, pp. 566-568.29. 何立东,袁新,尹新,蜂窝密封减振机理的实验研究,中国电机工程学报,2001, Vol. 21, No. 10, pp. 24-27. EI: . 何立东,袁新,尹新,刷式密封研究的进展,中国电机工程学报,2001, Vol. 21, No. 12, pp. 28-32, 53. EI: . 何立东,袁新,何丽娜,离心压缩机扩容改造中的转子动平衡,热能动力工程,2001, Vol. 16, No. 2, pp. 202-204. EI: . 张士杰,袁新,叶大均,非线性双方程湍流模型用于风力机翼型分离流动模拟,太阳能学报,2001, Vol. 22, No. 2, pp. 162-166. EI: RN 47828733. 何立东,袁新,非线性密封流体激振研究及进展,中国电机工程学报,2001, Vol. 21, No. Supplement, pp. 264-268.34. 张士杰,袁新,叶大均,多级轴流压气机全工况特性数值模拟,工程热物理学报,2002, Vol. 23, No. 2, pp. 167-170.35. 张士杰,袁新,叶大均,跨声速轴流压气机级全工况三维流场数值分析,推进技术,2002, Vol. 23, No. 3, pp. 209-212. EI: . 金琰,袁新,二维机翼振动非定常流场的数值模拟,清华大学学报(自然科学版),2002, Vol. 42, No. 5, pp. 684-687. EI: . 金琰,袁新,申炳録,机翼大攻角下失速颤振的气动弹性研究,工程热物理学报,2002, Vol. 23, No. 5, pp. 573-575. EI: . 金琰,袁新,应用流固耦合数值方法研究机翼的射流减振技术,空气动力学学报,2002, Vol.20, No.3, pp. 267,273. EI: . 金琰,袁新,机翼颤振及射流减振技术的气动分析,太阳能学报,2002, Vol.23, No.4, pp. 403,407. EI: . 林智荣,袁新,并行计算用于叶轮机械流场特性分析,工程热物理学报,2002, Vol. 23, No. 6, pp. 695-698.41. 王会社,钟兢军,王松涛,王仲奇,袁新,叶片弯曲对压气机叶栅气动性能影响的数值模拟,空气动力学学报,2002, Vol.20, No.4, pp. 470-476. EI: . 王会社,袁新,岳国强,钟兢军,王仲奇,弯曲叶片积叠线对压气机叶栅气动性能的影响,航空动力学报,2002, Vol.17, No.3, pp. 327-331.43. 赖宇阳,袁新,基于遗传算法和逐次序列规划的环形叶栅基迭优化,工程热物理学报,2003, Vol. 24, No. 1, pp. 52-54.国内期刊44. 袁新,热力叶轮机械内部的全三维复杂流动数值模拟研究点滴, 上海汽轮机, 2000, No. 1, Ser. No. 74, pp. 12-19.45. 袁新,林智荣,张士杰,张宏武,徐纲,并行计算用于叶轮机械流场特性全工况分析,清华同方技术通讯,2001, No. 1 (Ser. No. 5), pp. 37-41.46. 袁新,林智荣,集群计算机系统用于叶轮机械通流部分全三维设计分析,燃气轮机技术,2002, Vol. 15, No. 1 (Ser. No. 55), pp. 1-6.

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