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SIMULATION OF TETHERED UNDERWATER KITES MOVING IN THREE DIMENSIONS FOR POWER GENERATION

机译:三维发电三维移动的束缚水下风筝仿真

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In this paper, a numerical simulation of tether undersea kites (TUSK) used for power generation is undertaken. The effect of varying key design parameters in these systems is studied. TUSK systems consist of a rigid-winged kite, or glider, moving in an ocean current. One proposed TUSK concept uses a tethered kite which is connected by a flexible tether to a support structure with a generator on a surface buoy. The numerical simulation models the flow field in a three-dimensional domain near the rigid undersea kite wing by solving the full Navier-Stokes equations. A moving computational domain method is used to reduce the computational run times. A second-order corrector-predictor method, along with Open Multi-Processing (OpenMP), is employed to solve the flow equations. In order to track the rigid kite, which is a rectangular planform wing with a NACA 0021 airfoil, an immersed boundary method is used. The tension force in the elastic tether is modeled by a simple Hooke's law, and the effect of tether damping is added. PID control methods are used to adjust the kite pitch, roll and yaw angles during power (tether reel-out) and retraction (reel-in) phases to obtain the desired kite trajectories. During the reel-out phase the kite moves in successive cross-current motions in a figure-8 pattern, the tether length increases and power is generated. During reel-in the kite motion is along the tether, and kite hydrodynamic forces are reduced so that net positive power is produced. The effects of different key design parameters in TUSK systems, such as the ratio of tether to current velocity, and tether retraction velocity, are then further studied. System power output, kite trajectories, and vorticity flow fields for the kite are also determined.
机译:本文采用了用于发电的系绳下划线风筝(TUSK)的数值模拟。研究了这些系统中不同关键设计参数的影响。塔斯克系统由刚性的风筝或滑翔机组成,在海洋电流中移动。一个提出的托斯概念使用龙舌尿,其通过柔性系绳连接到支撑结构,在表面浮标上具有发电机。通过求解全Navier-Stokes方程,数值模拟模拟刚性Undersea风筝机翼附近的三维域中的流场。移动计算域方法用于减少计算运行时间。采用二阶校正器预测器方法以及开放式多处理(OpenMP)来解决流动方程。为了跟踪具有Naca 0021翼型的矩形平面翼的刚性风筝,使用浸入的边界方法。弹性系绳中的张力由简单的胡克定律建模,并加入系绳阻尼的效果。 PID控制方法用于在功率(系绳卷绕)和缩回(卷轴)相期间调节风筝间距,滚动和偏航角,以获得所需的风筝轨迹。在卷绕阶段期间,风筝在图8模式中在连续的交叉电流运动中移动,产生系绳长度增加和功率。在卷轴期间,风筝运动沿着系绳,并且风筝流体动力力减小,从而产生净正极功率。然后进一步研究不同关键设计参数在托斯系统中的影响,例如系绳与当前速度的比率,以及系绳缩进的比率。还确定了风筝的系统电源输出,风筝轨迹和涡旋流场。

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