...
首页> 外文期刊>The Transactions of the Royal Institution of Naval Architects >MEASURED LOADING RESPONSE OF MODEL MOTION CONTROL STERN TABS
【24h】

MEASURED LOADING RESPONSE OF MODEL MOTION CONTROL STERN TABS

机译:运动控制斯特恩三角翼的测得载荷响应

获取原文
获取原文并翻译 | 示例

摘要

Active trim tabs are commonly used as part of the ride control systems of high-speed craft. This paper investigates the lift characteristics of rectangular stern tabs that are commonly fitted to INCAT wave-piercer catamarans. A test apparatus was developed to enable the testing of a model scale trim tab in a circulating water tunnel in the University of Tasmania hydraulics laboratory. The magnitude and location of the lift force produced by the tab were measured over a range of tab angles and flow velocities. From this the lift coefficient of the tab was calculated and the performance of the tab under varying conditions was analysed. The lift force produced by the tab was shown to increase with velocity and tab angle as expected, with the lift coefficient of the tab increasing linearly with tab angle and remaining relatively constant with increases in flow velocity. The magnitude of the measured lift coefficient was lower than had been previously estimated in shallow water tests and the force was found to act forward of the tab hinge, indicating that much of the lift force generated by the tab is due to the increased pressure on the underside of the hull forward of the tab.
机译:主动装饰片通常用作高速航行器的行驶控制系统的一部分。本文研究了通常适用于INCAT冲孔双体船的矩形船尾翼片的升力特性。塔斯马尼亚大学水力学实验室开发了一种测试设备,可以在循环水隧道中测试模型比例调整片。由拉环产生的升力的大小和位置是在拉环角度和流速范围内测量的。由此计算出突舌的升力系数,并分析了在不同条件下突舌的性能。如图所示,翼片产生的升力随速度和翼片角度而增加,翼片的升力系数随翼片角度线性增加,并随着流速的增加而保持相对恒定。测得的升力系数的幅度低于先前在浅水测试中估计的升力系数,并且发现该力作用在翼片铰链的前方,这表明翼片产生的大部分升力是由于在翼片上的压力增加所致。标签前部的船体下方。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号