Proceedings of the First Mandalika International Multi-Conference on Science and Engineering 2022, MIMSE 2022 (Mechanical and Electrical) (MIMSE-M-E-I-2022)

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Analysis Aerodynamic Performance Airfoil WORTMANN FX63-137 in Different Reynolds Number

Authors
I. K. Wiratama1, *, I. M. Suartika1, I. W. Joniarta1, I. M. Mara1, I. M. Nuarsa1, Muammil Ansori1
1University of Mataram, Mataram, West Nusa Tenggara, Indonesia
*Corresponding author. Email: kwiratama@tm.ftunram.ac.id
Corresponding Author
I. K. Wiratama
Available Online 26 December 2022.
DOI
10.2991/978-94-6463-078-7_14How to use a DOI?
Keywords
Reynold Number; Angle of Attach; Stall; airfoil
Abstract

The investigation of flow behavior on the upper and lower surface airfoil was performed to know aerodynamic behaviors of airfoil in different Reynold Number. The more flexible simulation by using Computer Fluid Dynamic (CFD) has been used to analyze the behavior of flow which was addressed to application wind turbine blade in low Reynold Number. The aim of study was conducted to know the effecting of the stall behavior airfoil and parametric aerodynamic such as Lift Force (L), Drag Force (D), Lift Coefficient (CL), Drag Coefficient (CD), Lift Force over Drag Force (L/D) on various Reynold Number from 2,5 × 105, 5 × 105, 7,5 × 105 to 106. From the result simulation, it was found that the stall behavior for each Reynolds Number was at the same angle of attack, which was 24°. While the lift and drag forces are influenced by the Reynolds Number as the Reynolds Number getting bigger, the lift and drag forces increased. However, Reynolds Number did not affect the increase in the lift coefficient, drag coefficient, and L/D.

Copyright
© 2023 The Author(s)
Open Access
Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

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Volume Title
Proceedings of the First Mandalika International Multi-Conference on Science and Engineering 2022, MIMSE 2022 (Mechanical and Electrical) (MIMSE-M-E-I-2022)
Series
Advances in Engineering Research
Publication Date
26 December 2022
ISBN
978-94-6463-078-7
ISSN
2352-5401
DOI
10.2991/978-94-6463-078-7_14How to use a DOI?
Copyright
© 2023 The Author(s)
Open Access
Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

Cite this article

risenwbib
TY  - CONF
AU  - I. K. Wiratama
AU  - I. M. Suartika
AU  - I. W. Joniarta
AU  - I. M. Mara
AU  - I. M. Nuarsa
AU  - Muammil Ansori
PY  - 2022
DA  - 2022/12/26
TI  - Analysis Aerodynamic Performance Airfoil WORTMANN FX63-137 in Different Reynolds Number
BT  - Proceedings of the First Mandalika International Multi-Conference on Science and Engineering 2022, MIMSE 2022 (Mechanical and Electrical) (MIMSE-M-E-I-2022)
PB  - Atlantis Press
SP  - 125
EP  - 131
SN  - 2352-5401
UR  - https://doi.org/10.2991/978-94-6463-078-7_14
DO  - 10.2991/978-94-6463-078-7_14
ID  - Wiratama2022
ER  -