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航空宇航推进系

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刘小华

职务：航空宇航推进系副主任、长聘副教授、博导

电子邮件：Xiaohua-Liu@sjtu.edu.cn

办公地址：诸侯快讯导航ok1188诸侯快讯官方A321室

工作经历

时间	任职单位	职务
2024年-至今	诸侯快讯导航ok1188诸侯快讯官方	长聘副教授
2020年-2023年	诸侯快讯导航ok1188诸侯快讯官方	长聘教轨副教授
2018年-2019年	诸侯快讯导航ok1188诸侯快讯官方	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

研究方向

（1）压气机声共振的理论预测与模拟；

（2）先进航空发动机气动稳定性、主/被动控制；

（3）叶轮机械气动性能/噪声一体化设计。

主要科研项目

（1）主持国家自然科学基金、上海市自然科学基金等；

（2）主持燃气轮机/航空发动机相关企业等项目；

（3）参与国家重大专项、国家自然科学基金重点项目、国际合作项目等。

代表性论文专著

（1）Sun L, Yang J, Liu X, Sun D, Dong X. Diagnosis of Unsteady Disturbance Characteristics Induced by the Tip Leakage Vortex in a Compressor based on Data-driven Modal Decomposition Methods. Physics of Fluids. 2024. (accepted, in production).

（2）Lu J, Liu X. A theoretical Model of the Impedance at Blade Tip Clearance in Aeroengine Compressor. Aerospace Systems. 2024. (accepted, in production).

（3）Liu Y, Pan C, Liu X, Yang J. An Aerodynamic Investigation of the Last-Stage Turbine in an Upgraded Gas Turbine. ASME Journal of Fluids Engineering. 2024;146(6): 061202-1-12.

（4）Liu X, Wu Z, Si C, Yang J, Sun X. Role of Unsteady Tip Leakage Flow in Acoustic Resonance Inception of a Multistage Compressor. Chinese Journal of Aeronautics. 2023;36(10):165-81.

（5）Si C, Wu Z, Liu X. Simplified Numerical Models of the Unsteady Tip Leakage Flow in Compressor. Journal of Thermal Science. 2023;32(6):2386-1-14.

（6）Tao Q, Jin H, Liu X, Zhu Z. A Fast Computational Method of the Aerodynamic Performance of Fan and Booster with Inlet Distortion. Proceedings of the Institution of Mechanical Engineers Part C, Journal of Mechanical Engineering Science. 2023;237(1):67-82.

（7）Yang J, Feng X, Liu X, Peng T, Chen Z, Wang Z. The Suppression of Hump Instability inside a Pump Turbine in Pump Mode Using Water Injection Control. Processes. 2023;11(6):1647-1-17.

（8）Yang J, Feng X, Liao Z, Pan K, Liu X. Analysis on the Mechanism of Rotating Stall Inner a Pump Turbine in Pump Mode Based on the Proper Orthogonal Decomposition. ASME Journal of Fluids Engineering. 2023;145(9):091202-1-12.

（9）Yang J, Bai Z, Song C, Ding H, Chen M, Sun J, Liu X. Research on the Internal Flow Field of Left Atrial Appendage and Stroke Risk Assessment with Different Blood Models. Bioengineering. 2023;10(8):944-1-22.

（10）Qiu Z, Zhu Z, Liu X. An investigation of aerodynamic performance of aeroengine fan and booster under non-uniform inlet conditions. Aerospace Systems. 2023.(online)

（11）Yang J, Song C, Ding H, Chen M, Sun J, Liu X. Numerical study of the risk of thrombosis in the left atrial appendage of chicken wing shape in atrial fibrillation. Frontiers in Cardiovascular Medicine. 2022;9:985674-1-12.

（12）Li Y, Fang C, Liu X. Effect of tip injection on the flow characteristics of an aeroengine compressor rotor. Aerospace Systems. 2021;4(2):151-169.

（13）Liao Z, Yang J, Liu X, Hu W, Deng X. Analysis of Unsteady Flow Structures in a Centrifugal Impeller Using Proper Orthogonal Decomposition. Journal of Applied Fluid Mechanics. 2021;14(1):89-101.

（14）Yang J, Xie T, Liu X, Si Q, Liu J. Study of Unforced Unsteadiness in Centrifugal Pump at Partial Flow Rates. Journal of Thermal Science. 2021;30(1):88-99.

（15）Liu X, Teng J, Yang J, Sun X, Sun D, He C, Du J. Calculation of Stall Margin Enhancement with Micro-Tip Injection in an Axial Compressor. ASME Journal of Fluids Engineering. 2019;141(8):81109-1-10.

（16）Yang J, Liu J, Liu X, Xie T. Numerical Study of Pressure Pulsation of Centrifugal Pumps with the Compressible Mode. Journal of Thermal Science. 2019;28(1):106-114.

（17）Xie Z, Liu Y, Liu X, Lu L, Sun X. Effect of RANS Method on the Stall Onset Prediction by an Eigenvalue Approach. ASME Journal of Fluids Engineering. 2019;141(3). 031401-1-12.

（18）Yang J, Pavesi G, Liu X, Xie T, Liu J. Unsteady flow characteristics regarding hump instability in the first stage of a multistage pump-turbine in pump mode. Renewable Energy. 2018;127(11):377-385.

（19）Liu X, Willeke T, Herbst F, Yang J, Seume J. A Theory on the Onset of Acoustic Resonance in a Multistage Compressor. ASME Journal of Turbomachinery. 2018;140(8):81003-1-10.

（20）Yang J, Xie T, Giorgio P, Liu X, Liu J. Numerical Study on Rotating Characteristics of Unsteady Flow Inner Pump-turbine in Pump Mode. International Journal of Fluid Machinery and Systems. 2018;11(3):224-33.

（21）Xie Z, Liu Y, Liu X, Sun D, Lu L, Sun X. Computational Model for Stall Inception and Nonlinear Evolution in Axial Flow Compressors. AIAA Journal of Propulsion and Power. 2018;34(3):720-729.

（22）He C, Ma Y, Liu X, Sun D, Sun X. Aerodynamic Instabilities of Swept Airfoil Design in Transonic Axial-Flow Compressors. AIAA Journal. 2018;56(5):1878-93.

（23）Sun D, Nie C, Liu X, Lin F, Sun X. Further Investigation on Transonic Compressor Stall Margin Enhancement with Stall Precursor Suppressed Casing Treatment, ASME Journal of Turbomachinery. 2016;138(2): 021001-1-13.

（24）Sun X, Ma Y, Liu X, Sun D. Flow Stability Model of Centrifugal Compressors Based on Eigenvalue Approach. AIAA Journal. 2016;54(8): 2361-2376.

（25）Sun D, Liu X, Sun X. An Evaluation Approach for the Stall Margin Enhancement with Stall Precursor-Suppressed Casing Treatment. ASME Journal of Fluids Engineering. 2015;137(8): 081102-1-16.

（26）Liu X, Zhou, Y. P., Sun X, Sun D. Calculation of Flow Instability Inception in High Speed Axial Compressors Based on an Eigenvalue Theory, ASME Journal of Turbomachinery. 2015;137(6): 061007-1-9.

（27）Ma, Y. F., Liu X, Sun D, Sun X. 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.

（28）Liu X, Sun D, Sun X. Basic Studies of Flow-Instability Inception in Axial Compressors Using Eigenvalue Method. ASME Journal of Fluids Engineering. 2014;136(3): 031102-1-9.

（29）Sun X, Sun D, Liu X, Yu W, Wang X. A Theory of Compressor Stability Enhancement Using Novel Casing Treatment, Part I: Methodology. AIAA Journal of Propulsion and Power. 2014;30(5): 1224-1235.

（30）Sun D, Liu X, Jin D, Gui X, Sun X. A Theory of Compressor Stability Enhancement Using Novel Casing Treatment, Part II: Experiment. AIAA Journal of Propulsion and Power. 2014;30(5): 1236-1247.

（31）He C, Ma Y, Liu X, Sun D, and Sun X. Aerodynamic Instabilities of Swept Airfoil Design in Transonic Axial-Flow Compressors. AIAA Journal. 2018;56(5):1878-1893.

（32）Sun X, Liu X, Hou R, Sun D. A General Theory of Flow Instability Inception in Turbomachinery. AIAA Journal. 2013;51(7): 1675-1687.

（33）Liu X, Sun D, Sun X, Wang X. Flow Stability Model for Fan/Compressors with Annular Duct and Novel Casing Treatment. Chinese Journal of Aeronautics. 2012;25(2): 143-154.

（34）Liu X, Hou R, Sun D, Sun X. 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.

（35）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.

（36）孙大坤, 刘小华, 孙晓峰. 非定常机匣处理扩稳实验研究. 工程热物理学报. 2008: 29(12): 2022-2026.

（37）刘小华，周燕佩，孙大坤，马云飞，孙晓峰. 基于特征值理论的轴流跨声速压气机失稳预测. 航空学报. 2014;35(11): 2979-2991.

（38）董旭，刘小华，孙大坤，孙晓峰. 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. 2014; 35(9): 2411-2425.

（39）谢喆, 柳阳威, 刘小华, 孙晓峰, 陆利蓬. 旋转进口畸变频率对跨声速压气机稳定性影响的数值研究. 航空发动机. 2015; 41(5): 1-7.

（40）孙晓峰, 何晨, 刘小华, 马云飞, 孙大坤. 航空压气机流动稳定性预测研究进展. 推进技术. 2017;38(10): 2172-2185.