首页> 外文期刊>Journal of ship production and design >Comparison of Model-Scale and Full-scale Deceleration of a Fully Skirted Air Cushion Vehicle in Sideslip
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Comparison of Model-Scale and Full-scale Deceleration of a Fully Skirted Air Cushion Vehicle in Sideslip

机译:侧滑全裙式气垫车模型减缩与比例减缩的比较

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摘要

This article provides experimental results and shows comparisons of 90° sideslip performance of a fully skirted air cushion vehicle using theoretical predictions, 1/12th model-scale data, and full-scale data. The goal is to establish a relation among the three data sets and draw conclusions for use in future predictions. First, this article presents results and analysis of tow tank data obtained in late 2008. Then, the Froude scaled data are used to obtain an empirical drag coefficient. A comparison is made between this approach and a theoretical prediction proposed in previous work. An iterative, one-dimensional deceleration algorithm is then constructed using the coefficients to predict the deceleration of a full-scale craft having similar skirt characteristics. The predictions are performed for three craft weights and the resulting deceleration rates as a function of Froude number are presented. Data obtained from full-scale testing are then compared with the results of both the model-based algorithm and the theoretical prediction. In general, the model-based simulation overpredicts the deceleration rate for a full-scale craft, whereas the theoretical prediction is more accurate. The model simulation is recomputed using a developed correction factor and is plotted against the theoretical and full-scale deceleration, revealing favorable results. Lastly, a review of the technique is described and recommendations for improvements and following work are provided.
机译:本文提供了实验结果,并使用理论预测,1/12的模型比例数据和比例数据对全裙式气垫车的90°侧滑性能进行了比较。目标是在这三个数据集之间建立关系,并得出结论以用于将来的预测。首先,本文介绍了在2008年末获得的拖船数据的结果和分析。然后,使用Froude比例数据获得了经验阻力系数。将这种方法与先前工作中提出的理论预测进行了比较。然后,使用这些系数构造一个迭代的一维减速算法,以预测具有相似裙边特性的全尺寸飞行器的减速。对三个飞行器重量进行了预测,并给出了作为Froude数函数的最终减速度。然后,将从全面测试获得的数据与基于模型的算法和理论预测的结果进行比较。通常,基于模型的模拟会过度预测全尺寸飞行器的减速率,而理论预测则更为准确。使用已开发的校正因子重新计算模型仿真,并针对理论和满量程减速度进行绘制,从而显示出令人满意的结果。最后,描述了对该技术的回顾,并提供了改进建议和后续工作。

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