李琳恺
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[1]李琳恺,顾蕴松,黄紫,彭振钧,张宗源,雷雨.双合成射流前体非对称涡控制技术及模型自由飞实验验证.[J]:实验流体力学,2023,37(4):96-104
[2]Shuai Luo,Linkai Li,Keming Cheng,Yunsong Gu,Ruishan Fang,Wanbo Wang.Active flow control of a supercritical airfoil and flap with sweeping jets.[J]:Applied Sciences,2023,13(18):10166
[3]孙蓉,李琳恺,顾蕴松,罗帅.基于表面分布式压力的车载气动力感知技术:实验流体力学,2023
[4]Linchuan Tian,Hui Hu,Linkai Li,Haiyang Hu.Experimental Study of Dynamic Ice Accretion Process over Rotating Aeroengine Fan Blades:JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
[5]郭江龙,顾蕴松,罗帅,李琳恺.基于表面压力信息的空间流向涡识别方法研究:航空学报,2022,44(6):191-202
[6]Chi S,Gu Y,Gong D,Li L.Investigation of thrust vector angle control law based on micro turbojet engine:AIP Advances
[7].Mechanism of hysteresis and uncontrolled deflection in jet vectoring control based on Coanda effe....[J]:Physics of Fluids,34(8):084107
[8]Linkai Li,gys,李强,何梦杰.Suppression of Low-Reynolds-Number Flow Separation by Controlling the Laminar Separation Bubble w...:Journal of Aerospace Engineering,2022
[9]LK. Li,,Y. Liu, LC. Tian, HY. Hu, H. Hu,XJ. Liu, I. Hogate and A. Kohli.An experimental study on a hot-air-based anti-/de-icing system for aero-engine inlet guide vanes.[J]:Applied Thermal Engineering,2020,167:114778
[10]LK. Li,,Y. Liu and H. Hu.An Experimental Study on Dynamic Ice Accretion Process over the Surfaces of Rotating Aero-Engine ....[J]:Experimental Thermal and Fluid Science,2019,109:109879
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