当前位置: X-MOL首页全球导师 国内导师 › 刘小华

个人简介

刘小华 职务:航空宇航推进系副主任、长聘教轨副教授、博导 工作经历 时间任职单位职务 2020年-至今 上海交通大学航空航天学院 长聘教轨副教授 2018年-2019年上海交通大学航空航天学院长聘教轨助理教授 2016年-2017年University of Hannover (德国)洪堡学者 2015年-2016年中国航发商发公司研发中心主管专员(挂职) 2015年-2016年中国民用航空发动机适航审定中心适航审定工程师 2013年-2014年 中国民航科学技术研究院 适航审定工程师 教育背景 时间 毕业院校 学历 2007年-2013年 北京航空航天大学 博士 2003年-2007年 北京航空航天大学 本科 主要科研项目 (1)主持国家自然科学基金青年项目、面上项目; (2)主持上海市自然科学基金面上项目; (3)参与国家自然科学基金重点项目、国际合作项目、民航局本级项目等若干。 荣誉奖励 2006 北京航空航天大学金质奖章; 2017 亚洲流体机械国际会议最佳论文奖; 2019 ICASSE国际会议最佳论文奖; 2019 上海交通大学航空航天学院优秀教师; 2019 上海交通大学学生社会实践优秀指导教师。

研究领域

(1)航空发动机气动稳定性的通用理论预测、主/被动控制; (2)航空压气机声共振的理论预测与模拟; (3)民用航空发动机适航技术。

近期论文

查看导师新发文章 (温馨提示:请注意重名现象,建议点开原文通过作者单位确认)

(1)Liu X. H., Teng J. F., Yang J., Sun X. F., Sun D. K., He C., Du J. (2019): Calculation of Stall Margin Enhancement With Micro-Tip Injection in an Axial Compressor, ASME Journal of Fluids Engineering, Vol. 141(8):81109-1-10. (2)Yang J., Liu J., Liu X. H., Xie T. (2019): Numerical Study of Pressure Pulsation of Centrifugal Pumps with the Compressible Mode, Journal of Thermal Science, Vol. 28(1):106-114. (3)Xie Zhe, Liu Y. W., Liu X. H., Sun D. K., Lu L. P., Sun X. F.(2018): Computational Model for Stall Inception and Nonlinear Evolution in Axial Flow Compressors, AIAA Journal of Propulsion and Power, Vol. 34(3):720-729. (4)Liu X. H., Willeke T., Herbst F., Yang J., Seume J. (2018): A Theory on the Onset of Acoustic Resonance in a Multistage Compressor, ASME Journal of Turbomachinery, Vol. 140(8):81003-1-10. (5)Liu, X. H., Zhou, Y. P., Sun, X. F., Sun, D. K. (2015): Calculation of Flow Instability Inception in High Speed Axial Compressors Based on an Eigenvalue Theory, ASME Journal of Turbomachinery, Vol. 137(6), 061007-1-9. (6)Sun, D. K., Nie, C. Q., Liu, X. H.*, Lin, F., Sun, X. F. (2016): Further Investigation on Transonic Compressor Stall Margin Enhancement with Stall Precursor Suppressed Casing Treatment, ASME Journal of Turbomachinery, Vol. 138(2), 021001-1-13. (7)Sun, X. F., Liu, X. H., Hou, R. W., Sun, D. K. (2013): A General Theory of Flow Instability Inception in Turbomachinery, AIAA Journal, Vol. 51(7), 1675-1687. (8)Liu, X. H., Sun, D. K., Sun, X. F. (2014): Basic Studies of Flow-Instability Inception in Axial Compressors Using Eigenvalue Method, ASME Journal of Fluids Engineering, Vol. 136(3), 031102-1-9. (9)Liu, X. H., Sun, D. K., Sun, X. F., Wang, X. Y. (2012): Flow Stability Model for Fan/Compressors with Annular Duct and Novel Casing Treatment, Chinese Journal of Aeronautics, Vol. 25(2), 143-154. (10)Sun, X. F., Ma, Y. F., Liu, X. H., Sun, D. K. (2016): Flow Stability Model of Centrifugal Compressors Based on Eigenvalue Approach, AIAA Journal, Vol. 54(8), 2361-2376. (11)Sun, D. K., Liu, X. H., Sun, X. F. (2015): An Evaluation Approach for the Stall Margin Enhancement with Stall Precursor-Suppressed Casing Treatment, ASME Journal of Fluids Engineering, Vol. 137(8), 081102-1-16. (12)Sun, X. F., Sun, D. K., Liu, X. H., Yu, W. W., Wang, X. Y. (2014): A Theory of Compressor Stability Enhancement Using Novel Casing Treatment, Part I: Methodology, AIAA Journal of Propulsion and Power, Vol. 30(5), 1224-1235. (13)Sun, D. K., Liu, X. H., Jin, D. H., Gui, X. M, Sun, X. F. (2014): A Theory of Compressor Stability Enhancement Using Novel Casing Treatment, Part II: Experiment, AIAA Journal of Propulsion and Power, Vol. 30(5), 1236-1247. (14)Dong, X., Liu, X. H., Sun, D. K., Sun, X. F. (2014): Experimental investigation on SPS casing treatment with bias flow, Chinese Journal of Aeronautics, Vol. 27(6), 1352-1362. (15)Xie, Z., Liu, Y. W., Liu, X. H., Sun, D. K., Lu, L. P., and Sun, X. F., (2018): A Computational Model for Stall Inception and Nonlinear Evolution in Axial Flow Compressors, AIAA Journal of Propulsion and Power, Vol. 34(3):720-729. (16)He, C., Ma, Y. F., Liu, X. H., Sun, D. K., and Sun, X. F., (2018): Aerodynamic Instabilities of Swept Airfoil Design in Transonic Axial-Flow Compressors. AIAA Journal, Vol.56(5):1878-1893. (17)Liu, X. H., Sun, D. K., Sun, X. F. (2010): A Model to Predict Stall Inception of Axial Flow Fan/Compressors with Annular Duct, 3rd International Symposium on Jet Propulsion and Power Engineering, No. 2010-ISJPPE-1053, Nanjing, China, Sep. 13-17, 2010. (18)Liu, X. H., Hou, R. W., Sun, D. K. Sun, X. F. (2011): Stall Inception Model for Fan/Compressors including the Effect of Three Dimensional Blade Shape, 10th International gas turbine congress, No. IGTC2011-ABS-0070, Osaka, Japan, Nov. 13-18, 2011. (19)Liu, X. H., Hou, R. W., Sun, D. K., Sun, X. F. (2012): Flow Instability Inception Model of Compressors Based on Eigenvalue Theory, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA-2012-4156, Atlanta, USA, Jul. 30-Aug.1, 2012. (20)Liu, X. H., Zhou, Y. P., Sun, X. F., Sun, D. K.(2014): Calculation of Flow Instability Inception in High Speed Axial Compressors, Proceedings of ASME Turbo Expo 2014, GT 2014-26436, Düsseldorf, Germany, Jun. 16-20, 2014. (21)Ma, Y. F., Liu, X. H., Sun, D. K., Sun, X. F. (2015): Numerical Prediction of Stall Inception in Centrifugal Compressor Using Eigenvalue Method, ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT2015-42590, Montréal, Canada, Jun. 15-19, 2015. (22)刘小华:《叶轮机流动稳定性通用理论与非定常机匣处理扩稳研究》,博士论文,导师:孙晓峰,北京航空航天大学,2013. (23)孙大坤, 刘小华, 孙晓峰(2008): 非定常机匣处理扩稳实验研究, 工程热物理学报, 29(12), 2022-2026. (24)刘小华,周燕佩,孙大坤,马云飞,孙晓峰(2014): 基于特征值理论的轴流跨声速压气机失稳预测,航空学报,35(11), 2979-2991. (25)董旭,刘小华,孙大坤,孙晓峰(2014):旋转畸变条件下新型机匣处理扩稳效果实验研究, 航空学报, 35(9), 2411-2425.

学术兼职

(1)德国洪堡学者; (2)ASME、GPPS等若干国际会议及学术期刊审稿专家。

推荐链接
down
wechat
bug