Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 11, 17 November 2023


Open Access | Article

The study the angle of attack and lift magnitude of a wing using COMSOL software

Runpeng Chen * 1 , Yongqi Zhao 2
1 University of Toronto
2 Stony Brook University

* Author to whom correspondence should be addressed.

Theoretical and Natural Science, Vol. 11, 156-159
Published 17 November 2023. © 2023 The Author(s). Published by EWA Publishing
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Citation Runpeng Chen, Yongqi Zhao. The study the angle of attack and lift magnitude of a wing using COMSOL software. TNS (2023) Vol. 11: 156-159. DOI: 10.54254/2753-8818/11/20230398.

Abstract

Angle of attack (A.O.A.) is defined as the angle at which the chord of an aircraft’s wing meets the relative wind. At low angles of attack, the wing could just create a small amount of lift, and it also experience a small amount of drag. As the A.O.A. increases, both lift and drag will increase. However, when the wing reaches a critical angle of attack, the lift it could produce will quickly decrease, since the separation of the air flow and the wing surface. The objective of this study is to find the relationship between the angle of attack and the lift coefficient(which is proportional to the lift it could produce) of the wing. And as a conclusion, we find that the A.O.A. increase, the lift coefficient will also increase, and if the inlet velocity, the wing’s surface area and the velocity remains constant, when the lift coefficient increase, the lift will also increase.

Keywords

angle of attack, lift and drag, stall.

References

1. “Angle of Attack Awareness,” Federal Aviation Administration. [Online]. Available: https://www.faa.gov/news/safety_briefing/2019/media/SE_Topic_19-06.pdf. [Accessed: 10-Mar-2023].

2. “The lift coefficient,” NASA. [Online]. Available: https://www.grc.nasa.gov/www/k12/VirtualAero/BottleRocket/airplane/liftco.html#:~:text=The%20lift%20coefficient%20Cl%20is,times%20the%20wing%20area%20A.&text=Here%20is%20a%20way%20to,and%20measure%20the%20lift%20produced. [Accessed: 10-Feb-2023].

3. “Comsol tutorial of flow around cylinder ,” bilibili, 28-Mar-2020. [Online]. Available: https://www.bilibili.com/video/BV1yi4y1b7dt?spm_id_from=333.337.search-card.all.click. [Ac-cessed: 05-May-2022].

4. P. Lyu, “How do I compute lift and drag?,” COMSOL, 16-Jun-2015. [Online]. Available: https://www.comsol.com/blogs/how-do-i-compute-lift-and-drag/. [Accessed: 18-Mar-2023].

5. Aerodynamics of flight . (2022). In Pilot’s Handbook of Aeronautical Knowledge (pp. 5-1-5-4). essay, Washington, D.C.: U.S. Department of Transportation, Federal Aviation Admin-istration, Flight Standards Service.

Data Availability

The datasets used and/or analyzed during the current study will be available from the authors upon reasonable request.

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Volume Title
Proceedings of the 2023 International Conference on Mathematical Physics and Computational Simulation
ISBN (Print)
978-1-83558-133-9
ISBN (Online)
978-1-83558-134-6
Published Date
17 November 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/11/20230398
Copyright
17 November 2023
Open Access
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited

Copyright © 2023 EWA Publishing. Unless Otherwise Stated