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	Aerodynamic control of evaporative self-assembly in colloidal droplets 期刊论文 OAI收割 INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2025, 卷号: 239, 页码: 11 作者: Zhang C(张晨); Zheng ZY(郑中玉); Yan BF(严炳蜚); Xue J(薛健); Lan D(蓝鼎) \| 收藏 \| 浏览/下载：4/0 \| 提交时间：2025/02/24 Aerodynamic control Evaporative self-assembly Shear flow Coffee ring effect
	Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文 OAI收割 AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18 作者: Guo SQ(郭帅旗); Liu W(刘文); Zhang CA(张陈安); Liu Y(刘洋); Wang FM(王发民) \| 收藏 \| 浏览/下载：10/0 \| 提交时间：2024/02/05 Hypersonic waverider Aerodynamic model Symbolic regression Bluntness effect
	Prediction of coupling effect between pantograph and tunnel resulting from car body vibration using an aerodynamic and multi-body dynamic coupling approach 期刊论文 OAI收割 VEHICLE SYSTEM DYNAMICS, 2023 作者: Ji ZL(纪占玲); Guo Y(郭易); Guo DL(郭迪龙); Yang GW(杨国伟); Mao, Jun \| 收藏 \| 浏览/下载：15/0 \| 提交时间：2023/06/15 Coupling effect between pantograph and tunnel high-speed trains car body vibration aerodynamic and multi-body dynamic coupling pantograph
	Motion stability of high-speed maglev systems in consideration of aerodynamic effects: a study of a single magnetic suspension system 期刊论文 OAI收割 ACTA MECHANICA SINICA, 2017, 卷号: 33, 期号: 6, 页码: 1084-1094 作者: Wu H(吴晗); Zeng XH(曾晓辉); Yu Y(余杨) \| 收藏 \| 浏览/下载：30/0 \| 提交时间：2017/12/27 High-speed Maglev System Critical Speed Aerodynamic Effect Motion Stability
	Thermal-optical analysis for optical window under high Mach flight condition (EI CONFERENCE) 会议论文 OAI收割 2012 International Conference on Optoelectronics and Microelectronics, ICOM 2012, August 23, 2012 - August 25, 2012, Changchun, China Zhong C.; Ding Y.; Fu J. 收藏 \| 浏览/下载：21/0 \| 提交时间：2013/03/25 When the airborne platform where installed the optical window is in high Mach flight condition. The aerodynamic heating effect which will influence optical properties of optical window becomes very obvious. This special flight condition will change shape refractive index and also refractive index distribution of optical window due to the generated high axial temperature gradient. To ensure image quality of aerial remote sensor the present paper does thermal-optical analysis for optical window under high Mach flight condition. Then on this basis do simulations according to theoretical analysis and boundary conditions derived from practical assumptions in order to get the final conclusions. 2012 IEEE.
	Dome design and coupled thermal-mechanical analysis of supersonic missile (EI CONFERENCE) 会议论文 OAI收割 2009 International Conference on Optical Instruments and Technology, OIT 2009, October 19, 2009 - October 22, 2009, Shanghai, China Xing-qiao A.; Qun W.; Hong-guang J. 收藏 \| 浏览/下载：56/0 \| 提交时间：2013/03/25 A review of high-speed flow pressure and aerodynamic heating effect on Supersonic missile's dome is given. The dome should have excellent properties in optical mechanical and chemical characteristics. A design of dome on supersonic mode is described according to tactical guide line of a missile. The dome made of quartz which is about 8mm thick and 141mm in window diameter. To check up the reliability of the dome a reasonable finite element model (FEM) of dome is established and a thermal-mechanical Analysis to the dome by finite element software NASTRAN has carried on through these can obtained the distribution of temperature field and stress field when the speed is 2.3Ma. The results indicated that the stress was concentrated in the joint of the dome end and the Missile Section and the maximum stress was 16.4Mpa. The stress of other nodes was smaller than the allowable stress of quartz glass. Reference to the results of the analysis a lightweight revision to the dome structural dimension and a new method of dome fixing have put forward which can reduce the stress concentration. 2009 SPIE.