基本介紹
- 中文名：屈秋林
- 出生日期：1979年8月3日
- 畢業院校：北京航空航天大學
- 學位/學歷：博士
- 職業：教師
- 專業方向：流體力學
- 任職院校：北京航空航天大學
個人經歷,教育經歷,工作經歷,社會兼職,主講課程,研究方向,學術成果,榮譽獎項,
個人經歷
教育經歷
[1] 1998.9-2002.7
[2] 2002.7-2008.1
北京航空航天大學 | 流體力學 | 博士學位 | 博士研究生畢業
工作經歷
[1] 2008.1-2009.12
北京航空航天大學 | 航空科學與技術國家實驗室（籌） | 講師
[2] 2010.1-至今
北京航空航天大學 | 航空科學與工程學院 | 先後任講師、副教授
[3] 2013.2-2014.2
美國聖路易斯華盛頓大學 | 機械工程與材料科學系 | 訪問學者
[4] 2016.3-2017.4
美國聖路易斯華盛頓大學 | 機械工程與材料科學系 | 高級訪問學者
社會兼職
[1] 美國航空航天學會副會士（Associate Fellow of AIAA）
[2] Aerospace Science and Technology副主編
[3] Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering副主編
[4] SAE International Journal of Aerospace副主編
[5] 《氣體物理》青年編委
[6] AIAA Journal, Journal of Aircraft, Aerospace Science and Technology等期刊的審稿人
主講課程
承擔國家精品課《空氣動力學》的中文和英文教學工作。
研究方向
[1] 地面效應空氣動力學研究，包括地效飛行器近地面/水面巡航飛行的靜態地面效應、飛機起飛爬升和降落進近過程中的動態地面效應、艦載機艦面起降過程中的突變地面效應、鳥類及昆蟲飛行中的撲翼地面效應，系列研究成果發表在AIAA Journal，Journal of Aircraft，Aerospace Science and Technology等航空期刊中。
[2] 飛機水上迫降適航符合性驗證技術研究，提出採用整體動格線技術模擬飛機和水面相對運動的計算方法，目前該方法已經成功套用於ARJ21、MA700飛機的迫降性能評估，為其通過適航提供支撐。
[3] 積水跑道滑跑濺水適航符合性驗證技術研究，搭建用於滑跑濺水性能評估的數值平台，該平台精度優於荷蘭NLR的CRspray平台，目前已經成功用於指導ARJ21飛機的適航驗證。
學術成果
截止目前，共發表SCI論文43篇、EI論文63篇，獲授權發明專利13項，多次擔任AIAA會議分會場主席。
論文
[1] Gao BS, Qu QL, and Agarwal RK. Aerodynamics of a Transonic Airfoil in Ground Effect, Journal of Aircraft, 2018, DOI: 10.2514/1.C034998.
[2] Zhang W, Liu PQ, Guo H, and Qu QL. Multi-scale entropy analysis and conditional sampling of the velocity increment in a transitional boundary layer, Communications in Nonlinear Science and Numerical Simulation, 2019, 67: 303-313.
[3] Zhang X, Liu PQ, Qu QL, Wang R and Agarwal RK. Effects of Froude number and geometry on water entry of a 2D ellipse, Journal of Hydrodynamics, 2018, 30(4): 738-749.
[4] Liu ZC, Liu PQ, Hu TX and Qu QL. Experimental investigations on high altitude airship propellers with blade planform variations, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232(16): 2952-2960.
[5] Zhang YJ, Liu PQ, Qu QL, Liu T, and Hu TX. Characteristics and model of the initial spray caused by an aircraft elastic tire rolling on the water-contaminated runway, Aerospace Science and Technology, 2018, 79: 610-624.
[6] Zhang X, Liu PQ, Qu QL, Zhao YK, Hu TX, and Agarwal RK. Numerical Analysis of the Pressure Peak Position Shift with Deadrise Angle in Two-Dimensional Wedge Water Entry, ASME Journal of Fluids Engineering, 140(11): 111101.
[7] Jiang RP, Tian Y, Liu PQ, Gao SQ, and Qu QL. Transonic Buffet Control Research on Supercritical Wing Using Rear-Mounted Bump, Journal of Aerospace Engineering, 2018, 31(5): 04018053.
[8] Qu QL, Liu T, Liu PQ and Agarwal RK. Simulation of Water Spray Generated by Pneumatic Aircraft Tire on Flooded Runway, Journal of Aircraft, 2018, 55(4): 1700-1708.
[9] Zhao KB, Liu PQ, Qu QL, Ma PC and Hu TX. Flow physics and chine control of the water spray generated by an aircraft rigid tire rolling on contaminated runways, Aerospace Science and Technology, 2018, 72: 49-62.
[10] Zhao KB, Liu PQ, Qu QL, Lin L, Lv J, Ding W and Agarwal RK. Numerical Simulation of Aircraft Tire-Generated Spray and Engine Ingestion on Flooded Runways, Journal of Aircraft, 2017, 54(5): 1840-1848.
[11] Qin YP, Liu PQ, Qu QL, and Hu TX. Wing/canard interference of a close-coupled canard configuration in static ground effect, Aerospace Science and Technology, 2017, 69: 60-75.
[12] Tian Y, Feng PH, Liu PQ, Hu TX, and Qu QL. Spoiler Upward Deflection on Transonic Buffet Control of Supercritical Airfoil and Wing, Journal of Aircraft, 2017, 54(3): 1227-1233.
[13] Qu QL, Wang R, Guo H, Liu PQ, and Agarwal RK. Study of Water Impact of an Elastic Cylindrical Shell, AIAA Journal, 2016, 54(10): 3296-3303.
[14] Qu QL, Ma PC, Liu PQ, Li SW, Agarwal RK. Numerical Study of Transient Deformation and Drag Characteristics of a Decelerating Droplet, AIAA Journal, 2016, 54(2): 490-505.
[15] Qu QL, Liu CS, Liu PQ, Guo BD, Agarwal RK. Numerical Simulation of Water-Landing Performance of a Regional Aircraft, Journal of Aircraft, 2016, 53(6): 1680-1689.
[16] Qu QL, Zhang F, Liu PQ, Agarwal RK. Numerical Simulation of Water Spray Caused by a Rolling Airplane Tire, Journal of Aircraft, 2016, 53(1): 182-188.
[17] Qin YP, Liu PQ, Qu QL, Guo H. Numerical study of aerodynamic forces and flow physics of a delta wing in dynamic ground effect, Aerospace Science and Technology, 2016, 51: 203-221.
[18] Chen MQ, Liu PQ, Guo H, Qu QL. Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration, Journal of Aircraft, 2016, 53(1): 217-230.
[19] Wang YP, Liu, PQ, Hu TX, Qu QL. Investigation of co-rotating vortex merger in ground proximity, Aerospace Science and Technology, 2016, 53: 116–127.
[20] Wang WH, Liu PQ, Tian Y, Qu QL. Numerical study of the aerodynamic characteristics of high-lift droop nose with the deflection of fowler flap and spoiler, Aerospace Science and Technology, 2016, 48: 75–85.
[21] Liu ZC, Liu PQ, Qu QL, Hu TX. Effect of Advance Ratio and Blade Planform on the Propeller Performance of a High Altitude Airship， Journal of Applied Fluid Mechanics, 2016, 9(6): 2993-3000.
[22] Qu QL, Zuo PY, Wang W, Liu PQ, Agarwal RK. Numerical Investigation of the Aerodynamics of an Airfoil in Mutational Ground Effect, AIAA Journal, 2015, 53(10): 3144-3154.
[23] Qu QL, Wang W, Liu PQ, Agarwal RK. Airfoil Aerodynamics in Ground Effect for Wide Range of Angles of Attack, AIAA Journal, 2015, 53(4): 1048-1061.
[24] Qu QL, Hu MX, Guo H, Liu PQ, Agarwal RK. Study of Ditching Characteristics of Transport Aircraft by Global Moving Mesh Method, Journal of Aircraft, 2015, 52(5): 1550-1558.
[25] Qu QL, Lu Z, Guo H, Liu PQ, Agarwal RK. Numerical Investigation of the Aerodynamics of a Delta Wing in Ground Effect, Journal of Aircraft, 2015, 52(1): 329-340.
[26] Qin YP, Qu QL, Liu PQ, Tian Y, Lu Z. DDES study of the aerodynamic forces and flow physics of a delta wing in static ground effect, Aerospace Science and Technology, 2015, 43: 423–436.
[27] Guo H, Huang QM, Liu PQ, Qu QL. Effects of local high-frequency perturbation on a turbulent boundary layer by synthetic jet injection, Fluid Dynamics Research, 2015, 43, Paper No. 045501.
[28] Qu QL, Jia X, Wang W, Liu PQ, Agarwal RK. Numerical Simulation of the Flowfield of an Airfoil in Dynamic Ground Effect, Journal of Aircraft, 2014, 51(5): 1659-1662.
[29] Qu QL, Lu Z, Liu PQ, Agarwal, RK. Numerical Study of Aerodynamics of a Wing-in-Ground-Effect Craft, Journal of Aircraft, 2014, 51(3): 913-924.
[30] Qu QL, Jia X, Wang W, Liu PQ, Agarwal RK. Numerical study of the aerodynamics of a NACA 4412 airfoil in dynamic ground effect, Aerospace Science and Technology, 2014, 38: 56-63.
[31] Guo BD, Liu PQ, Qu QL, Wang JW. Effect of pitch angle on initial stage of a transport airplane ditching, Chinese Journal of Aeronautics, 2013, 26(1): 17-26.
[32] Guo H, Li C, Qu QL, Liu, PQ. Attractive fixed-point solution study of a shell model for turbulent convection, Science China-Physics Mechanics & Astronomy, 2013, 56(5): 995-1003.
[33] Guo H, Li C, Qu QL, Liu, PQ. Attractive fixed-point solution study of shell model for homogeneous isotropic turbulence, Applied Mathematics and Mechanics-English Edition, 2013, 34(3): 259-268.
[34] Guo H, Chen JJ, Qu QL, Liu PQ. Generation of spatial atmospheric turbulence field in aircraft motion simulation based on refined similarity hypothesis, Science China-Technological Sciences, 2011, 54(1): 244-250.
榮譽獎項
2015年入選國家留學基金委“未來科學家項目”，2017年入選北航“青年人才拔尖計畫”，2018年入選國家民航局“民航科技創新人才推進計畫”。2017年獲得教育部“高等學校科學研究優秀成果獎（技術發明獎）”一等獎（排名：5/6）、2018年獲得北京市“高等教育教學成果獎”二等獎（排名：3/9）。2019年獲得北航校級青年教師講課比賽二等獎。
