期刊文献+
共找到6篇文章
< 1 >
每页显示 20 50 100
Dynamic modeling and analysis of vortex filament motion using a novel curve-fitting method 被引量:2
1
作者 Chang-Joo Kim Soo Hyung Park +1 位作者 Sang Kyung Sung Sung-Nam Jung 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2016年第1期53-65,共13页
Applications of a novel curve-fitting technique are presented to efficiently predict the motion of the vortex filament, which is trailed from a rigid body such as wings and rotors. The gov- erning equations of the mot... Applications of a novel curve-fitting technique are presented to efficiently predict the motion of the vortex filament, which is trailed from a rigid body such as wings and rotors. The gov- erning equations of the motion, when a Lagrangian approach with the present curve-fitting method is applied, can be transformed into an easily solvable form of the system of nonlinear ordinary dif- ferential equations. The applicability of Bezier curves, B-spline, and Lagrange interpolating polyno- mials is investigated. Local Lagrange interpolating polynomials with a shift operator are proposed as the best selection for applications, since it provides superior system characteristics with minimum computing time, compared to other methods. In addition, the Gauss quadrature formula with local refinement strategy has been developed for an accurate prediction of the induced velocity computed with the line integration of the Biot-Savart law. Rotary-wing problems including a vortex ring problem are analyzed to show the efficiency, accuracy, and flexibility in the applications of the pro- posed method. 展开更多
关键词 AERODYNAMICS Biot-Savart law Curve-fitting method Free-vortex wake Rotary wing vortex filament
原文传递
飞机尾涡对的三维失稳快速模拟方法
2
作者 徐梓铭 李栋 +1 位作者 蔡金延 李沛繁 《空气动力学学报》 北大核心 2025年第1期95-104,I0002,共11页
飞机尾流是制约机场飞行间隔缩短的重要因素之一,然而当前的尾流演化数值模拟和经验模型均无法兼顾尾流演化的时效性和准确性,不利于管制机场尾流间隔。考虑到飞机尾流由飞机尾涡对主导,而动力学失稳又是飞机尾涡耗散的主要机制,本文提... 飞机尾流是制约机场飞行间隔缩短的重要因素之一,然而当前的尾流演化数值模拟和经验模型均无法兼顾尾流演化的时效性和准确性,不利于管制机场尾流间隔。考虑到飞机尾流由飞机尾涡对主导,而动力学失稳又是飞机尾涡耗散的主要机制,本文提出基于曲率修正涡丝法的飞机尾涡对失稳快速模拟方法。通过三次样条插值得到涡段中点坐标,将直涡段处理为弯曲涡段,同时考虑涡段对自身控制点的诱导作用,实现涡丝法诱导速度的曲率修正。另外,给出了涡丝法模拟飞机尾涡对周期条件的处理方法,大幅提升了涡丝法模拟飞机尾涡失稳的计算精度。数值实验结果表明,考虑曲率修正的涡丝法能够以较低的计算成本实现快速预测尾涡对长波失稳,并且失稳增长率、涡丝倾角均与理论值吻合良好。在施加不同强度的湍流扰动后,本文方法模拟得到的涡对快速耗散时间与理论值吻合较好,尤其对于中弱强度的湍流扰动,本文方法预测结果更为准确。 展开更多
关键词 飞机尾涡 动力学失稳 涡丝法 曲率修正 大气湍流
在线阅读 下载PDF
圆射流中拟序涡配对的数值模拟 被引量:1
3
作者 林建忠 吴法理 刘中秋 《力学季刊》 CSCD 北大核心 2001年第4期408-415,共8页
用三维涡丝法结合涡丝的增加与合并技术,对不可压圆射流场,数值模拟了在扰动中加入次谐波后流场拟序涡的配对,配对情况与实验结果一致,通过对不同时刻涡量图的比较与分析,给出了次谐波初始强度对涡配对的影响,初始强度越大,涡配对出现越... 用三维涡丝法结合涡丝的增加与合并技术,对不可压圆射流场,数值模拟了在扰动中加入次谐波后流场拟序涡的配对,配对情况与实验结果一致,通过对不同时刻涡量图的比较与分析,给出了次谐波初始强度对涡配对的影响,初始强度越大,涡配对出现越早,涡配对位置越往上游移动;同时还得到了基波与次谐波初始相位差和涡配对的关系,没有相位差时,次谐波增长最快,相位差增加时,涡配对的速度降低。说明控制次谐波的初始强度和基波与次谐波的相位差,能起到控制圆射流剪切层乃至控制整个射流场的目的。 展开更多
关键词 圆射流 拟序涡配对 涡丝法 数值模拟 拟序涡 不可压 扰动 次谐波 涡量图 相位差
在线阅读 下载PDF
The Full Non‑linear Vortex Tube‑Vorton Method: the pre‑stall condition
4
作者 Jesus Carlos Pimentel‑Garcia 《Advances in Aerodynamics》 2024年第1期324-355,共32页
The present hybrid vortex tube-vorton method is based entirely on the Full Multi-wake Vortex Lattice Method(FMVLM)concepts,which means detaching vorticity with pre-cise vortex strength and orientation along all separa... The present hybrid vortex tube-vorton method is based entirely on the Full Multi-wake Vortex Lattice Method(FMVLM)concepts,which means detaching vorticity with pre-cise vortex strength and orientation along all separation lines between each discretized element of a shell-body,including all external edges.Since the classic Vortex Particle Method(VPM)is unstable by itself because it does not conserve the total amount of circulation as time evolves(Kelvin’s circulation theorem),an isolated Vortex(regular-ized)Filament Method(VFM)approach is implemented to obtain advection of vorti-city,while the induced velocity field is obtained through its corresponding full vorton cloud.Further,a novel vortex squeezing/stretching scheme for such a vortex cylinder-sphere approach is proposed based on variation in time for vortex volumes in order to precisely(zero residual)conserve both circulation and vorticity at each time step(for each detached vortex element),while the viscous effect can be accounted for via the Core Spreading Method(CSM). 展开更多
关键词 vortex methods vortex filament method Vorton method Meshless methods Detached flow Low aspect ratio aerodynamics
原文传递
轴对称射流中涡运动的三维涡丝模拟 被引量:1
5
作者 刘中秋 林建忠 石兴 《科技通报》 北大核心 2002年第4期270-275,280,共7页
用三维涡丝法对轴对称不可压射流进行了数值模拟 ,描述了轴对称射流在外加扰动下产生的拟序结构随时间的发展 .文中应用了涡丝的增加与合并技术 ,模拟了在基波扰动作用下涡的卷起 ,以及在扰动中加入次谐波后涡的配对 .通过对不同时刻涡... 用三维涡丝法对轴对称不可压射流进行了数值模拟 ,描述了轴对称射流在外加扰动下产生的拟序结构随时间的发展 .文中应用了涡丝的增加与合并技术 ,模拟了在基波扰动作用下涡的卷起 ,以及在扰动中加入次谐波后涡的配对 .通过对不同时刻涡量图的比较与分析 ,说明扰动中的基波导致涡的卷起 ,次谐波控制着涡的配对 。 展开更多
关键词 轴对称射流 中涡运动 三维涡丝 拟序结构 数值模拟
在线阅读 下载PDF
Kinematics and forces of a flexible body in Karman vortex street 被引量:5
6
作者 WANG SiYing JIA LaiBing YIN XieZhen 《Chinese Science Bulletin》 SCIE EI CAS 2009年第4期556-561,共6页
Experiments of a flexible filament in the wake of a cylinder and in free stream were conducted in a vertical soap film tunnel. The experiments distinctly visualized the movement of the filament. Based on the experimen... Experiments of a flexible filament in the wake of a cylinder and in free stream were conducted in a vertical soap film tunnel. The experiments distinctly visualized the movement of the filament. Based on the experimental kinematic results, a 2-d panel method was used to calculate the forces acting on the filament. The experiment and numerical results revealed that different from that in free stream, the filament in Karman vortex street flapped at the same frequency as the vortex street, and with smaller amplitude and larger curvature. The filament suffered an evident thrust in Karman vortex street, while a drag appeared in the case of free stream. The dependence of the drag coefficient on the phase relation between the movement of the filament and the Karman vortex street was also studied. 展开更多
关键词 卡曼旋涡流 柔韧细丝 肥皂膜 阻力系数
在线阅读 下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部