A Coupled Viscous/Potential-Flow Method for the Prediction of Propulsor-Induced Maneuvering Forces

C. L. Warren, T. E. Taylor, J. Kerwin
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引用次数: 9

Abstract

A technique for the analysis of propulsor-induced maneuvering forces on the surface and underwater vehicles has been developed. The method is capable of modeling general propulsors but is especially suited to complex integrated propulsors and their highly contracting stern flows. Integrated propulsors exhibit strong interactions of the blade-rows, duct, and vehicle stern. The method described herein is a robust means to analyze propulsor-induced maneuvering forces, including those arising from complex propulsors. The heart of the maneuvering force prediction is a three-dimensional, unsteady lifting surface method for the calculation of blade forces on both rotors and stators. The lifting surface method includes features that are important for the modeling of complex propulsors. Temporally-varying forces are computed for a blade-row rotating in a spatially-varying flow field. The spatially-varying flowfield around a maneuvering vehicle is obtained by coupling the unsteady lifting-surface method with a three-dimensional, time-averaged Reynolds Averaged Navier-Stokes viscous flow solver. The coupled technique allows the designer to compute maneuvering forces while accounting for effective wake issues and propulsor-hull interactions. Issues important to the coupling of a potential-flow method and a three-dimensional viscous flow solver are discussed. Verification of the method has been performed on a variety of geometries and vehicles. Two examples are shown. Preliminary results show that the method is able to compute propulsor-induced maneuvering forces for such vehicles. The results suggest that this maneuvering force prediction method has great potential for the propulsor designer.
一种预测推进器机动力的粘性/势流耦合方法
提出了一种分析水面和水下航行器上由推进器引起的机动力的方法。该方法能够对一般推进器进行建模,但特别适用于复杂的集成推进器及其高度收缩的尾流。整体式推进器表现出桨叶排、风道和船艉之间强烈的相互作用。本文所描述的方法是一种分析由螺旋桨引起的机动力,包括由复杂螺旋桨引起的机动力的鲁棒方法。机动力预测的核心是一种三维非定常升力面方法,用于计算转子和定子上的叶片力。升力面方法包含了对复杂推进器建模很重要的特征。计算了叶片排在空间变流场中旋转时的变力。将非定常升力面法与三维时均Reynolds平均Navier-Stokes粘性流动求解器相结合,得到了机动飞行器周围空间变化的流场。耦合技术允许设计者计算机动力,同时考虑有效的尾流问题和推进器与船体的相互作用。讨论了势流法与三维粘性流动求解器耦合的重要问题。该方法已在各种几何形状和车辆上进行了验证。下面给出了两个例子。初步结果表明,该方法能够计算出该类飞行器由推进器引起的机动力。结果表明,这种机动力预测方法对推进器设计人员具有很大的应用潜力。
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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