An informal introduction to basic concepts of aerodynamics: part II: thin airfoils and wings in incompressible fluid flows

Mohamed Hafez

首页> 外文期刊>International Journal of Aerodynamics >An informal introduction to basic concepts of aerodynamics: part II: thin airfoils and wings in incompressible fluid flows

【24h】

An informal introduction to basic concepts of aerodynamics: part II: thin airfoils and wings in incompressible fluid flows

机译：空气动力学基本概念的非正式介绍：第二部分：不可压缩流体中的薄机翼和机翼

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

This paper is a sequel of part I. Here, thin airfoil theory for thickness and lifting problems are presented in terms of velocity components due to two dimensional source and vortex distributions. Flows around bodies of revolution are also treated using three dimensional sources and effects of small angle of attack are considered using cross flow analysis. Low and high aspect ratio wings are studied with different approximations. Viscous effects are included using velocity/vorticity formulation as well.

机译：本文是第一部分的续篇。这里，由于二维源和涡旋分布，根据速度分量提出了用于厚度和升力问题的薄翼型理论。旋转体周围的流动也使用三维源进行处理，并使用交叉流动分析来考虑小攻角的影响。低和高纵横比的机翼以不同的近似值进行研究。粘性效应也包括使用速度/涡度公式。

著录项

来源
《International Journal of Aerodynamics》 |2013年第4期|共37页
作者
Mohamed Hafez;
展开▼
作者单位

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类空气动力学;
关键词
Thin airfoil; Slender body; Slender wing; Lifting line theories; Blasius solution of boundary layer equations; Viscous/inviscid interaction; Velocity/vorticity formulation; Zonal approach;

机译：薄型翼型;细长的机身;细长的机翼;起重线理论;边界层方程的Brasius解;粘性/无粘性相互作用;速度/涡度公式化;区域法;

相似文献

外文文献
中文文献
专利

1. An informal introduction to basic concepts of aerodynamics: part II: thin airfoils and wings in incompressible fluid flows [J] . Mohamed Hafez International Journal of Aerodynamics . 2013,第4期

机译：空气动力学基本概念的非正式介绍：第二部分：不可压缩流体中的薄机翼和机翼
2. Aerodynamic Characteristics of a Thin Airfoil Cascade in an Ideal Incompressible Flow with Separation from the Leading Edges [J] . V. B. Kurzin, V. A. Yudin Fluid Dynamics . 2009,第2期

机译：从前缘分离的理想不可压缩流中的薄翼型叶栅的空气动力学特性
3. FUNDAMENTAL SOLUTIONS FOR THE PLANE-PARALLEL STEADY FLOW OF INCOMPRESSIBLE PERFECTLY CON- DUCTING FLUIDS PAST THIN AIRFOILS [J] . ADRIAN CARABINEANU Revue Roumaine de Mathematiques Pures et Appliquees . 1995,第3a4期

机译：不可压缩完美导流的薄型翼型平面平行稳态流动的基本解
4. An incompressible SPH method for simulating free surface flows of shear-thinning fluids [C] . Xiao-Yang Xu, Fang-An Deng International Conference on Mechanics and Mechanical Engineering . 2016

机译：一种用于模拟剪切稀疏流体的自由表面流动的不可压缩的SPH方法
5. A STUDY OF THE AERODYNAMIC PERFORMANCE OF WEIS-FOGH WINGS (UNSTEADY FLOW, BIOFLUIDDYNAMICS, INSECT FLIGHT). [D] . CHEN, HSUN HU. 1985

机译：魏斯雾翼的气动性能（非定常流动，生物流体动力学，昆虫飞行）的研究。
6. Effects of Leading Edge Defect on the Aerodynamic and Flow Characteristics of an S809 Airfoil [O] . Yan Wang, Xiaojing Zheng, Ruifeng Hu, -1

机译：前缘缺陷对S809翼型气动和流动特性的影响
7. A New Technique for Analysis of Unsteady Aerodynamic Responses of Cascade Airfoils with Blunt Leading Edge. Unsteady Aerodynamic Responses of the Cascade in Incompressible Flow. [O] . Ken-Ichi Funazaki, Kouichi Nihei, Atsushi Sasaki, 1993

机译：一种新技术，用于分析级联翼型与钝翼前缘级联翼型的空气动力学响应。不稳定流动级联的不稳定空气动力学响应。
8. The Two-dimensional Subsonic Flow of an Inviscid Fluid about an Aerofoil of Arbitrary Shape Part I. Incompressible Flow about a Symmetrical Aerofoil in a Channel or Free Stream. Part II. Incompressible Flow about an Asymmetric Aerofoil in a Free Stream. Part III. The Influence Factor Method of Calculating Incompressible Flow. Part IV. Compressible Flow. [R] . L. C. WOODS 1953

机译：关于任意形状翼型的Inviscid流体的二维亚音速流动。关于通道或自由流中对称翼型的不可压缩流动。第二部分。关于自由流中不对称翼型的不可压缩流动。第三部分。计算不可压缩流动的影响因素法。第四部分。可压缩流动。

An informal introduction to basic concepts of aerodynamics: part II: thin airfoils and wings in incompressible fluid flows

摘要

著录项

相似文献

相关主题

期刊订阅