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基于RANSE模型CFD预测E779A型螺旋桨空化及其在通用船体后的水动力性能
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作者 Mohammed Adnan Rizk Samir E.Belhenniche +1 位作者 Omar Imine omer kemal kinaci 《哈尔滨工程大学学报(英文版)》 CSCD 2023年第2期273-283,共11页
Ship propulsion performance heavily depends on cavitation,increasing the recent interest in this field to lower ship emissions.Academic research on the effects of cavitation is generally based on the open-water propel... Ship propulsion performance heavily depends on cavitation,increasing the recent interest in this field to lower ship emissions.Academic research on the effects of cavitation is generally based on the open-water propeller performance but the interactions of the cavitating propeller with the ship hull significantly affect the propulsion performance of the ship.In this study,we first investigate the INSEAN E779A propeller by a RANSE-based CFD in open-water conditions.The numerical implementation and the selected grid after sensitivity analysis partially succeeded in modeling the cavitating flow around the propeller.Satisfactory agreement was observed compared to experimental measurements.Then,using the open-water data as input,the propeller’s performance behind a full-scale ship was calculated under self-propulsion conditions.Despite being an undesired incident,we found a rare condition in which cavitation enhances propulsion efficiency.Atσ=1.5;the propeller rotation rate was lower,while the thrust and torque coefficients were higher. 展开更多
关键词 CAVITATION Marine propeller Propulsion efficiency Propeller-hull interaction INSEAN E779A
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Mathematical Model for Takeoff Simulation of a Wing in Proximity to the Ground
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作者 omer kemal kinaci 《Journal of Marine Science and Application》 CSCD 2016年第2期136-143,共8页
飞机飞结束到从提高的效率由于的扎根的利益减少导致拖并且增加的电梯。在这研究,一个数学模型被开发用一个反复的边界元素方法(IBEM ) 和有限差别计划在地面附近模仿一个翅膀的起飞。二独立亚代码和母亲代码,启用在亚代码之间的通讯... 飞机飞结束到从提高的效率由于的扎根的利益减少导致拖并且增加的电梯。在这研究,一个数学模型被开发用一个反复的边界元素方法(IBEM ) 和有限差别计划在地面附近模仿一个翅膀的起飞。二独立亚代码和母亲代码,启用在亚代码之间的通讯,被开发为 Wing-In-Ground (假发) 效果的自激解决。在翅膀上施加的空气动力学的力量被第一亚代码用 IBEM 计算,并且翅膀的垂直排水量由用有限差别计划的第二亚代码是计算的。二亚代码和罐头在秒以内为翅膀和操作高度的气体动力学解决的母亲代码命令。发达代码系统被用来为一个 NACA6409 翅膀的力量,速度,和排水量解决在一 40,和 20 ? 展开更多
关键词 数学模型 数值模拟 近地面 机翼 起飞 空气动力学 有限差分格式 有限差分方法
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