CFD Analysis of NACA 2421 Aerofoil at Several Angles of Attack

Varatharajan R Madhanraj; Dilip A Shah

首页> 外文期刊>Journal of Aeronautics & Aerospace Engineering >CFD Analysis of NACA 2421 Aerofoil at Several Angles of Attack

【24h】

CFD Analysis of NACA 2421 Aerofoil at Several Angles of Attack

机译：NACA 2421机翼在多个迎角上的CFD分析

获取原文

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

In this paper NACA 2421 Aerofoil is analyzed at several angles of attack ranging from -200 to 200 and with the Reynolds number at 1.8 × 105 and the velocity are 20 m/s. The co-efficient of lift and drag are compared with the standard values in the literature. Variation of pressure co-efficient is plotted in the form of contour. The aerofoil is designed in ANSYS and it is imported to Computational Fluid Dynamics and the variations of CL and CD with respect to various angles of attack is analyzed.

机译：在本文中，NACA 2421翼型在-200到200的多个迎角下进行了分析，雷诺数为1.8×105，速度为20 m / s。将升力和阻力系数与文献中的标准值进行比较。压力系数的变化以轮廓形式绘制。机翼是在ANSYS中设计的，并将其导入计算流体动力学，并分析了CL和CD相对于各种迎角的变化。

著录项

来源
《Journal of Aeronautics & Aerospace Engineering》 |2019年第1期|共4页
作者
Varatharajan R Madhanraj; Dilip A Shah;
展开▼
作者单位

展开▼
收录信息
原文格式 PDF
正文语种
中图分类航空;
关键词

相似文献

外文文献
中文文献
专利

1. Take-off characteristics for NACA 4612 aerofoil in a twin-wing configuration with optimum angles of attack [J] . Kenneth L. Witcher, Ian R. McAndrew, Elena Vishnevskaya MATEC Web of Conferences . 2018,第3期

机译：双翼配置中具有最佳迎角的NACA 4612机翼的起飞特性
2. Experimental Analysis of a NACA 0021 Airfoil Section Through 180-Deg Angle of Attack at Low Reynolds Numbers for Use in Wind Turbine Analysis [J] . Holst D., Church B., Pechlivanoglou G., Journal of Engineering for Gas Turbines and Power . 2019,第4期

机译：用于风力涡轮机分析的低雷诺数下NACA 0021翼型截面通过180度迎角的实验分析
3. On the prospects of improving the numerical analysis of symmetric airfoils at low Reynolds numbers and high angles of attack by a LES approach: the case of NACA0021 profile [J] . Simone Giaccherini, Filippo Mariotti, Lorenzo Pinelli, E3S Web of Conferences . 2020,第10期

机译：关于改善低雷诺数对称翼型数值分析的前景，LES方法的高攻击角度：NaCA0021简介的情况
4. CFD Analysis of Responses of Two-Equation Turbulence Models for Flow over NACA 0012, NACA 4412 and S809 Aerofoils [C] . S. Sahoo, S. Maity International Conference on Recent Innovations and Developments in Mechanical Engineering . 2020

机译：NACA 0012，NACA 4412和S809机翼流量的两方程湍流模型的CFD分析
5. MEASUREMENT OF TRUE ANGLE OF ATTACK AND TRUE ANGLE OF SIDESLIP BY SENSING THE MOTIONS OF AN AIRCRAFT. [D] . SMETANA, FREDERICK OTTO. 1961

机译：通过感测飞机的运动来测量攻击的真实角度和侧滑的真实角度。
6. The PELskin project-part V: towards the control of the flow around aerofoils at high angle of attack using a self-activated deployable flap [O] . Marco E. Rosti, Laura Kamps, Christoph Bruecker, -1

机译：PELskin项目第五部分：使用自激活可展开襟翼以大迎角控制翼型周围的流动
7. CFD Analysis of NACA 2421 Aerofoil at Several Angles of Attack [O] . Varatharajan R Madhanraj, Dilip A Shah 2019

机译：NACA 2421 Aeroy oil在几个攻击角度的CFD分析
8. Propeller induced angles of attack and section angles of attack for the NACA 10-(3)(066)-03, 10-(3)(049)-03, 10-(3)(090)-03, 10-(5)(066)-03, and 10-(0)(066)-03 propellers [R] . Igoe, William, B, Davidson, Robert E 1952

机译：NaCa 10-（3）（066）-03,10-（3）（049）-03,10-（3）（090）-03,10-（5）的螺旋桨诱导迎角和截面迎角）（066）-03和10-（0）（066）-03螺旋桨

CFD Analysis of NACA 2421 Aerofoil at Several Angles of Attack

摘要

著录项

相似文献

相关主题

期刊订阅