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在槽道艇的槽道下方装上首尾水翼以及在艇尾装上尾压浪板对艇的阻力及航态有较好的改善效果。通过对4种不同尺度、不同排水量的阻力性能、航态进行试验分析,得出了有利于阻力、航态的水翼翼型、水翼安装角、水翼安装位置,尾压浪板的安装角及其与水翼最佳配合的结论。 相似文献
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尾压浪板对高速艇阻力性能的影响 总被引:4,自引:0,他引:4
在高速艇上采用尾压浪板后,对减少艇体阻力常会得到较满意的结果。本文主要介绍上海交通大学船模试验池的有关试验结果,并分析了尾压浪板对艇体阻力的影响。得出以下几点结论:(1)排水量长度系数 C_D=D/((L/10)~3)是影响压浪板减阻效果的主要参数,当C_D>2.0,采用尾压浪板一般可收到减阻效果。(2)在 C_D≥2.0的范围内,高速排水量艇采用压浪板后所能得到的阻力收益大体可按下式进行估算:(ΔR_T)/(R_T)(%)=1.6 1.45C_D(3)尾压浪板的长度以船长的1~2%为宜。 相似文献
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本文介绍了高速流水推进双体船“徐福”号艉压浪板攻角变化对航态与航速影响的实船试验情况,指出合理采用可调攻角艉压浪板是调整圆舭艇航态,提高航速的一种简便有效的方法。 相似文献
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文章介绍了高速艇上水翼减阻的原理以及三种不同类型的高速艇上加装水翼的技术方案及其达到的减阻效果,并给出了滑行艇首部加装水翼(即翼滑艇)后整船阻力的估算方法。基于三维非线性涡格法,建立了单独水翼/水翼组合体/多水翼系统的水动力性能理论计算方法,计算结果与试验结果吻合较好,可作为翼滑艇阻力估算中单独水翼水动力性能的计算方法。算例结果表明,文中的方法可用于单独水翼/水翼组合体/多水翼系统和滑行艇加装减阻水翼的初步技术方案设计。 相似文献
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基于CFD技术,以排水型高速船Model 5b为模型,寻求改善高速船阻力性能的尾压浪板新形式。首先尾压浪板新形式的确定在静水条件下进行,然后在波浪条件下验证该压浪板的阻力性能。基于CFD软件建立三维数值波浪水池,静水条件下采用切割体网格技术预报船模的阻力性能。波浪条件下数值水池入口采用直接造波方法,尾部采用人工阻尼消波方法,自由面采用VOF方法处理,采用重叠网格技术预报船模的阻力性能以及运动响应。确定一种比常规压浪板阻力性能优良的分段式压浪板,为船舶节能附体的研究提供参考。 相似文献
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研究了单体小水线面水翼复合型高速船翼航状态的稳性原理。运用水翼艇的有关算法,推导了该船型翼船状态复原力矩的计算方法,讨论了不同水民办型式及升力与浮力的不同比例对其翼航状态稳性的影响,为该船型的研究和设计提供了依据。 相似文献
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Prandtl’s lifting line theory was generalized to the lifting problem of a three-dimensional hydrofoil in the presence of a free surface. Similar to the classical lifting theory, the singularity distribution method was utilized to solve two-dimensional lifting problems for the hydrofoil beneath the free surface at the air-water interface, and a lifting line theory was developed to correct three-dimensional effects of the hydrofoil with a large aspect ratio. Differing from the classical lifting theory, the main focus was on finding the three-dimensional Green function of the free surface induced by the steady motion of a system of horseshoe vortices under the free surface. Finally, numerical examples were given to show the relationship between the lift coefficient and submergence Froude numbers for 2-D and 3-D hydrofoils. If the submergence Froude number is small free surface effect will be significant registered as the increase of lift coefficient. The validity of these approaches was examined in comparison with the results calculated by other methods. 相似文献
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Nowadays, several stern devices are attracting a great deal of attention. The control surface is an effective apparatus for improving the hydrodynamic performance of planing hulls and is considered an important element in the design of planing hulls. Control surfaces produce forces and a pitching moment due to the pressure distribution that they cause, which can be used to change the running state of high-speed marine boats. This work elaborates a new study to evaluate the hydrodynamic performance of a planing boat with a trim tab and an interceptor, and optimizes them by using an optimization algorithm. The trim tab and the interceptor have been used to optimize the running trim and motion control of semi-planing and planing boats at various speeds and sea conditions for many years. In this paper, the usage of trim tab is mathematically verified and experimental equations are utilized to optimize the performance of a planing boat at a specificd trim angle by using an optimization algorithm. The genetic algorithm(GA) is one of the most useful optimizing methods and is used in this study. The planing boat equations were programmed according to Savitsky's equations and then analyzed in the framework of the GA-based optimization for performance improvement of theplaning hull. The optimal design of trim tab and interceptor for planing boat can be considered a multiobjective problem. The input data of GA include different parameters, such as speed, longitudinal center of gravity, and deadrise angle. We can extract the best range of forecasting the planing boat longitudinal center of gravity, the angle of the trim, and the least drag force at the best trim angle of the boat. 相似文献
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粒子群算法在翼型剖面优化中的应用 总被引:1,自引:0,他引:1
为设计出具有良好升阻比性能的翼型剖面,采用智能优化领域新兴的粒子群优化算法(PSO)结合面元法对翼型进行优化设计。文中给出了PSO算法的数学模型及其在翼型优化设计中的主要计算过程,并以Naca66mod翼型为原型进行设计。获取了翼型优化过程中每一步处的翼型剖面形状、翼型表面压力系数分布以及翼型的升力系数、阻力系数和最大厚度比,结果分析表明经过优化后的翼型与原型相比,具有升力系数增加,阻力系数减小这一有利的特征改变。同时采用CFD方法对两种翼型进行数值模拟计算,获得同上的结论,进而验证了PSO方法在翼型优化设计中的可行性。 相似文献
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介绍了由作者设计的双体水翼船和船模试验研究情况。试验中,对船模的一些主要要素进行了变化,得出了它们对船模和影响的一些规律。 相似文献
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解三维水翼绕流的下潜涡环栅格法 总被引:2,自引:1,他引:1
在包含于机翼表面内的某次表面及尾涡面上分布法向偶极子,在翼面上满足物面边界条件,建立了解三维机翼绕流的下潜涡环栅格法.考虑到非线性的自由液面边界条件,用下潜涡环栅格法求解水翼绕流问题.通过算例验证了方法的正确性和程序的可靠性.本方法可用于水翼及水下安定翼和各种舵的水动力计算. 相似文献
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基于粒子群算法的水翼剖面优化设计 总被引:1,自引:1,他引:0
水翼是船舶设计和各种水中运动装置设计的重要组成部分,在船舶海洋工程领域的应用十分广泛.采用粒子群优化算法(PSO)对三维水翼翼型进行了以提高升阻比为目标的优化设计.翼型由解析函数线性叠加法表示,目标函数和粒子的适应度由基于面元法的流场数值解来提供.整个优化计算过程较传统的优化方法原理简单,计算量小,优化后的水翼型能较原翼型的水动力性能有明显改善.优化结果验证了粒子群优化算法结合面元法在水翼剖面优化设计中的可行性,对今后水翼剖面优化设计有一定借鉴意义。 相似文献
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