Theoretical and Computational Investigation on Swept Back Wing using CFD Method

IF 2.8 4区生物学

3 Biotech Pub Date : 2022-12-01 DOI:10.46632/jame/1/3/4

Rohit Bindal, Ankit Kumar Mishra

引用次数: 0

Abstract

The principles of flight deals with the motion of air and forces acting on an aircraft. The theoretical aspects of aircraft deals with four different forces. The main aim of the study was to analyse the Swept Back Wing for Supersonic and Hypersonic Mach Regimes at various angles of attack. The geometry and analysis were done using Ansys-Fluent. Calculations were done for constant air velocity altering only the angle of attack. The findings present up the contours of pressure and velocity along with evaluation of lift, drag and its coefficients

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后掠翼的CFD理论与计算研究

飞行原理涉及空气的运动和作用在飞机上的力。飞机的理论方面涉及四种不同的力。研究的主要目的是分析后掠翼在不同攻角下的超音速和高超音速马赫状态。使用Ansys-Fluent进行几何和分析。在恒定气流速度下进行了计算，只改变了迎角。研究结果给出了压力和速度的轮廓，并对升力、阻力及其系数进行了评估

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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来源期刊

3 Biotech BIOTECHNOLOGY & APPLIED MICROBIOLOGY-

自引率

0.00%

发文量

314

期刊介绍： 3 Biotech publishes the results of the latest research related to the study and application of biotechnology to: - Medicine and Biomedical Sciences - Agriculture - The Environment The focus on these three technology sectors recognizes that complete Biotechnology applications often require a combination of techniques. 3 Biotech not only presents the latest developments in biotechnology but also addresses the problems and benefits of integrating a variety of techniques for a particular application. 3 Biotech will appeal to scientists and engineers in both academia and industry focused on the safe and efficient application of Biotechnology to Medicine, Agriculture and the Environment.