地效飞行器的涡流晶格 CFD 应用和建模验证

Q3 Engineering

WSEAS Transactions on Fluid Mechanics Pub Date : 2024-02-09 DOI:10.37394/232013.2024.19.5

Karl Zammit, Howard Smith, Noel Sierra Lobo, Ioannis K. Giannopoulos

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引用次数: 0

摘要

本文探讨了涡流格计算流体动力学方法在利用地面效应模拟飞机近地飞行中的应用。计算结果与现有的分析公式相关联，并以公共领域的实验数据为基准。以俄罗斯 A-90 Orlyonok Ekranoplan 机翼为基础，进行了案例空气动力学设计研究。该研究为利用快速空气动力学结果生成涡流晶格 CFD 方法推进地效飞机周转概念和初步设计时间提供了验证和确认步骤。

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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Vortex Lattice CFD Application and Modeling Validation for Ground Effect Aircraft

This paper explores the application of vortex lattice computational fluid dynamics method capability to model aircraft flight near to ground, utilizing the ground effect. Computational results were correlated with existing analytic formulations and benchmarked against experimental data from the public domain. A case aerodynamics design study was formed, based on the Russian A-90 Orlyonok Ekranoplan wing. The study provided a verification and a validation step towards advancing ground effect aircraft turnaround conceptual and preliminary design time, using the rapid aerodynamics results generation vortex lattice CFD method.

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来源期刊

WSEAS Transactions on Fluid Mechanics Engineering-Computational Mechanics

CiteScore

1.50

自引率

0.00%

发文量

期刊介绍： WSEAS Transactions on Fluid Mechanics publishes original research papers relating to the studying of fluids. We aim to bring important work to a wide international audience and therefore only publish papers of exceptional scientific value that advance our understanding of this particular area. The research presented must transcend the limits of case studies, while both experimental and theoretical studies are accepted. It is a multi-disciplinary journal and therefore its content mirrors the diverse interests and approaches of scholars involved with multiphase flow, boundary layer flow, material properties, wave modelling and related areas. We also welcome scholarly contributions from officials with government agencies, international agencies, and non-governmental organizations.