Effect of Model Propeller Trailing Edge Details on Powering Performance

T. J. Michael, S. Jessup
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引用次数: 1

Abstract

Until recently, model propellers tested at the US Navy's David Taylor Model Basin (DTMB) incorporated relatively sharp trailing edges without fall scale features such as anti-singing trailing edges. These propellers have shown good agreement between design calculations and model measurements. With the advent of NURBS surface representation of model propeller geometry, new propeller models have been manufactured with fall scale trailing edge details. Problems have arisen in achieving predicted open water performance. Discrepancies have been attributed to trailing edge flows over beveled edges, and variations in trailing edge shape due to manufacturing problems. The analysis included detailed trailing edge measurements, an open water test. and panel method computations.
模型螺旋桨尾缘细节对动力性能的影响
直到最近,在美国海军的大卫·泰勒模型盆地(DTMB)测试的螺旋桨模型都采用了相对锋利的后缘,没有防唱后缘等降尺度特征。这些螺旋桨在设计计算和模型测量之间表现出良好的一致性。随着NURBS表面表示模型螺旋桨几何的出现,新的螺旋桨模型已制造与下降规模后缘细节。在实现预期的开放水域性能方面出现了一些问题。差异归因于斜边上的尾缘流动,以及由于制造问题而导致的尾缘形状的变化。分析包括详细的尾缘测量和开放水域测试。并进行面板法计算。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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