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Numerical Simulation of Seaplane Wave Ground Effect with Crosswind 被引量:3
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作者 LI Yanghui FU Xiaoqin +1 位作者 CHEN Jichang TONG Mingbo 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2021年第S01期1-9,共9页
Under the absolute coordinate system, the unsteady Reynolds averaged Navier-Stokes(URANS)equations and the k-ω SST turbulence model are solved using the finite volume method to simulate the aerodynamic characteristic... Under the absolute coordinate system, the unsteady Reynolds averaged Navier-Stokes(URANS)equations and the k-ω SST turbulence model are solved using the finite volume method to simulate the aerodynamic characteristics of large seaplane flying with the ground-effect above wavy surface. The velocity inlet wave-making method and the volume of fluid model are used to accurately simulate the linear regular waves and to precisely capture the free surface. This paper studies the influence of the sideslip angle on the aerodynamic characteristics of large seaplane when it is cruising above wavy water. The results show that the wave surface mainly affects the pressure distribution on the lower surface of the wing. When the sideslip angle varies from 0° to 8°,the varying of frequency of aerodynamic forces is consistent with the wave encounter frequency,and both periods are 0.6 s. With the increase of the sideslip angle,the lift coefficient and the pitching moment coefficient decrease. However,when the sideslip angle is smaller than 4°,the decrease amplitude is small,and the significant decrease occurs above 4° and during the whole process of the change of sideslip angle,the aerodynamic fluctuation amplitude is almost unchanged. As the drag coefficient increases with the increase of sideslip angle,significant increase also occurs when the value is greater than4°,and the fluctuation amplitude does not show any correlations. The rolling moment coefficient and yaw moment coefficient increase with the increase of the sideslip angle,and the fluctuation amplitudes of both increase linearly with the increase of the sideslip angle. 展开更多
关键词 two-phase flow wing-in-ground(wig)effect volume of fluid(VOF)model velocity-inlet boundary wave maker
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地效翼船纵向稳定性与操纵性研究 被引量:3
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作者 张红玲 楼连根 周伟麟 《上海交通大学学报》 EI CAS CSCD 北大核心 1999年第3期361-364,共4页
纵向稳定性一直是地效翼船发展中面临的问题之一.以状态方程作为描述地效翼船的数学模型,研究了地效翼船在飞行状态下的纵向操纵性与稳定性.根据特征方程常数项系数,直接判定静稳定性,分析了主要气动导数对静稳定性的影响,认为C... 纵向稳定性一直是地效翼船发展中面临的问题之一.以状态方程作为描述地效翼船的数学模型,研究了地效翼船在飞行状态下的纵向操纵性与稳定性.根据特征方程常数项系数,直接判定静稳定性,分析了主要气动导数对静稳定性的影响,认为Cmz取接近于零的正数既有利于静稳定性又能简化静稳定性的判定条件.根据特征根,判定动稳定性,作出模态矢量图,并分析了三个模态的主要特性以及状态变量在各模态中的反映;分析了在从自由空间到地效区的过渡区域,忽略速度变化的四阶运动方程所得的动稳定性与五阶方程所得的动稳定性不一致的原因,指出在这一区域尤其要注意四阶方程的有效性.最后。 展开更多
关键词 地效翼船 稳定性 操纵性 纵向稳定性 水翼船
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基于盒式翼的地效飞行器气动布局概念设计 被引量:1
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作者 路容斐 蒋崇文 +3 位作者 高振勋 李椿萱 张江 欧平 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2017年第S1期6-11,共6页
根据地面效应的特点及相似准则,给出了基于展弦比、梢根比和机翼离水相对高度等参数的盒式翼外形简化设计原则。针对地效飞行器高度焦点配置,结合盒式翼外形简化设计原则,给出了盒式翼纵向位置的简化设计方案。针对盒式翼地效飞行器在... 根据地面效应的特点及相似准则,给出了基于展弦比、梢根比和机翼离水相对高度等参数的盒式翼外形简化设计原则。针对地效飞行器高度焦点配置,结合盒式翼外形简化设计原则,给出了盒式翼纵向位置的简化设计方案。针对盒式翼地效飞行器在起飞过程中的升阻特性,给出了发动机类型选择及动力配置的优选方案。针对地效飞行器的飞行特点,阐述了盒式翼地效飞行器机身和尾翼的设计要点。通过以上分析为基于盒式翼的地效飞行器气动布局概念设计提供了设计依据和参考。 展开更多
关键词 气动布局 概念设计 盒式翼 地效飞行器 地面效应
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四阶特征方程判定地效翼船动稳定性的适用范围 被引量:1
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作者 张红玲 黄国梁 周伟麟 《上海交通大学学报》 EI CAS CSCD 北大核心 2000年第1期80-82,共3页
在分析五阶方程各模态特性的基础上,通过特征多项式根与系数的关系,证明了四阶方程动稳定不能确保五阶方程一定动稳定;同时通过四次与五次特征多项式的分析比较,给出四阶方程作为五阶方程有效近似的判定准则,作出判定曲线,得到四阶方程... 在分析五阶方程各模态特性的基础上,通过特征多项式根与系数的关系,证明了四阶方程动稳定不能确保五阶方程一定动稳定;同时通过四次与五次特征多项式的分析比较,给出四阶方程作为五阶方程有效近似的判定准则,作出判定曲线,得到四阶方程适用的飞高范围,并分析了各气动导数的变化对动稳定性的影响。 展开更多
关键词 地效翼船 动稳定性 特征多项式 船舶动力学
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The future and technique challenges of high-speed ground effect vehicle enrolled in maritime transportation
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作者 Jianhong Sun Chenlu Wang +5 位作者 Daren Zheng Zhi Sun Hao Liu Zhuoran Sheng Shengrun Zhang Weidong Zhao 《Aerospace Traffic and Safety》 2024年第1期43-54,共12页
This paper presents a high-speed ground effect vehicle(HS-GEV)used specifically for maritime transportation.Given the limitations of current vessels,including various types of watercraft and high-speed boats,in fulfil... This paper presents a high-speed ground effect vehicle(HS-GEV)used specifically for maritime transportation.Given the limitations of current vessels,including various types of watercraft and high-speed boats,in fulfilling of needs in different maritime transportation scenarios,the HS-GEV emerges as a promising solution to address unmet requirements.To efficiently accomplish maritime transportation missions with quickness and safety,several critical features are emphasized,including short take-off on water,flight maneuverability and flight stability.The key techniques required to achieve these features,as well as recent progress highlights,are introduced.Following and promoting these crucial techniques is also suggested as a future step to improve HS-GEV performance.With its predominant features,the HS-GEV holds immense application value in enhancing a high-speed maritime transportation system that aligns with the evolving needs of the real world. 展开更多
关键词 HS-GEV Maritime Transportation Drag Reduction Combined Power wing-in-ground(wig)effect Ground effect vehicle(GEV)
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