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The Moments on a Tumblehome Hull Form Undergoing Forced Roll

机译:滚石船体船体形式的瞬间接受强迫滚动

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The prediction of large amplitude roll motions and capsize events has proven to be difficult and includes large uncertainty. One of the reasons for this is a lack of knowledge of hydrodynamic forces and moments for large roll angles. Currently, the equations used by numerical models to predict forces and moments due to roll motion are based on small roll amplitude experimental data. In 2005, the Carderock Division, Naval Surface Warfare Center (NSWC/CD) tested Model 5613 (Figure 1), a tumble-home hull form, with the primary objective of obtaining model-scale forced motion seakeeping data to provide information necessary to perform validation of surge, sway, heave, roll, pitch, and yaw forces and moments acting on a combatant hull during large amplitude motions and capsize events. The model was forced in roll with amplitudes ranging from 5 to 50 and roll periods from 1 s to 3 s, at 4 forward speeds. During the test, the model was forced in roll both with and without bilge keels, with freedom to pitch and heave. The model had the ability to be fixed in yaw or free to yaw (only the fixed in yaw data are discussed in this paper). By performing a least squares fit of the measured data to a linear one-degree-of-freedom roll equation, the added inertia and roll damping coefficients can be determined. The added inertia and roll damping coefficients are greatest in magnitude for the higher speeds. Also, the added inertia coefficient reaches a maximum value for roll amplitudes of 20-30, while the roll damping coefficient reaches a minimum value for amplitudes of 20-30. This paper further examines the trends of the forces and moments, as well as the roll damping and added inertia coefficients as they relate to the roll characteristics and model speed.
机译:已经证明了大幅度辊运动和胶囊化事件的预测是困难的并且包括大的不确定性。其中一个原因是缺乏对大辊角的流体动力力和时刻的知识。目前,数值模型使用的等式以预测由于滚动运动引起的力和时刻基于小的辊幅幅度实验数据。 2005年,Cardercock部门,海军表面战中心(NSWC / CD)测试模型5613(图1),一个翻滚家庭船体形式,具有获取模型规模的强制运动海守数据的主要目标,以提供所需的信息在大振幅动作期间验证浪涌,摇摆,升降,滚动,俯仰和横摆力和偏航力和在战斗机船体上的时刻。该模型被强制在辊中,其振幅从5到50且从1秒的辊周期升至4个前进速度。在测试期间,模型被迫滚动,无论是否有舱底龙骨,自由于俯仰和升降。该模型具有固定在偏航或自由偏差中的能力(本文仅讨论了固定的偏航数据)。通过执行测量数据的最小二乘拟合到线性一度自由度滚动方程,可以确定附加的惯性和辊阻尼系数。增加的惯性和卷筒阻尼系数对于更高的速度最大。此外,附加的惯性系数达到辊幅为20-30的最大值,而辊阻尼系数达到20-30的幅度的最小值。本文进一步研究了力量和时刻的趋势,以及卷起和添加惯性系数,因为它们涉及卷起特性和模型速度。

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