Proceedings of the 3rd Tarumanagara International Conference on the Applications of Social Sciences and Humanities (TICASH 2021)

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Generating the Coordinates and Graph of NACA 00xx AIRFOIL using PYTHON

Authors
Vishwas Gowda P N1, *, Vibha Shekar MC2, Bagus Mulyawan3
1U.G Student, Department of Mechanical Engineering, Cauvery Institute of Technology, Karnataka, India
2U.G Student, Department of Electronics & Communication Engineering, Cauvery Institute of Technology, Karnataka, India
3Faculty of Information Systems, Universitas Tarumanagara, Jakarta, Indonesia
Corresponding Author
Vishwas Gowda P N
Available Online 21 April 2022.
DOI
10.2991/assehr.k.220404.334How to use a DOI?
Keywords
Airfoil; Python; Computational fluid dynamics; Co-ordinates; Aerodynamics
Abstract

Python is a remarkable interpreted level, open-source, and higher-level general-purpose programming language. In this paper, Python is introduced as a regulated programming language as to make use of it to analyze engineering problems and extract results in the form of a document or in a systematic graphical representation. The purpose of this paper is to extract the coordinates of the 4-digit NACA (National Advisory Committee for Aeronautics) 0012 airfoil by solving the airfoil equation using python. The main intention of this spadework is to use python to simplify the calculation, extract the airfoil coordinates in the form of a CSV file, and generate the graph for the respective. The tiny changes in these airfoil designs can alter the overall efficiency of the plane or a turbine or another machine where this is used. Each airfoil has its own advantages and disadvantages depending upon the application of the airfoil. NACA 0012 is one of the basic airfoil shapes used in the airplanes. These airfoil designs help the plane in stability, speed control, and landing of the flight. The designed airfoils are tested for the fluid flow over the airfoil using computational fluid dynamics or simply fluid dynamics through which the efficiency or the suitability of the airfoil is checked.

Copyright
© 2022 The Authors. Published by Atlantis Press SARL.
Open Access
This is an open access article distributed under the CC BY-NC 4.0 license.

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Volume Title
Proceedings of the 3rd Tarumanagara International Conference on the Applications of Social Sciences and Humanities (TICASH 2021)
Series
Advances in Social Science, Education and Humanities Research
Publication Date
21 April 2022
ISBN
10.2991/assehr.k.220404.334
ISSN
2352-5398
DOI
10.2991/assehr.k.220404.334How to use a DOI?
Copyright
© 2022 The Authors. Published by Atlantis Press SARL.
Open Access
This is an open access article distributed under the CC BY-NC 4.0 license.

Cite this article

risenwbib
TY  - CONF
AU  - Vishwas Gowda P N
AU  - Vibha Shekar MC
AU  - Bagus Mulyawan
PY  - 2022
DA  - 2022/04/21
TI  - Generating the Coordinates and Graph of NACA 00xx AIRFOIL using PYTHON
BT  - Proceedings of the 3rd Tarumanagara International Conference on the Applications of Social Sciences and Humanities (TICASH 2021)
PB  - Atlantis Press
SP  - 2033
EP  - 2038
SN  - 2352-5398
UR  - https://doi.org/10.2991/assehr.k.220404.334
DO  - 10.2991/assehr.k.220404.334
ID  - PN2022
ER  -