首页> 外文期刊>Progress in Aerospace Sciences >Review of computational methods for aerodynamic analysis of iced lifting surfaces
【24h】

Review of computational methods for aerodynamic analysis of iced lifting surfaces

机译:覆冰提升面空气动力学分析计算方法综述

获取原文
获取原文并翻译 | 示例
           

摘要

Extensive experimental studies and associated reviews have been conducted to better understand the aerodynamic impact of iced lifting surfaces based on measurements. This review is a computational compliment to these previous studies to understand how well we can predict these aerodynamics. In particular, we focus on classifying three-dimensional computational fluid dynamic (CFD) studies that have analyzed the aerodynamic impact of ice accretion on lifting surface geometries over the past three decades. The classification considers and discusses: airfoil/wing geometry, ice shape, flow conditions, meshing type/technique, numerical schemes, turbulence model, and prediction accuracy (via experimental validation). The review culminates in an informed commentary on the current gaps of knowledge present with regards to predicting aerodynamics on iced lifting surfaces, and recommends strategies for the research community to use to help address these issues.
机译:已经进行了广泛的实验研究和相关的评估,以根据测量结果更好地了解结冰的举升表面的空气动力学影响。本文是对这些先前研究的计算补充,以了解我们对这些空气动力学的预测能力。尤其是,我们专注于对三维计算流体动力学(CFD)研究进行分类,这些研究分析了过去三十年来冰块积聚对举升表面几何形状的气动影响。该分类考虑并讨论了:机翼/机翼几何形状,冰形状,流动条件,啮合类型/技术,数值方案,湍流模型和预测精度(通过实验验证)。这篇评论的最后内容是就目前在预测冰上举升表面上的空气动力学方面存在的知识空白,进行有见地的评论,并为研究界推荐用于解决这些问题的策略。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号