Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser
This paper presents the design and construction of a small open jet wind tunnel without the contraction and diffuser. The wind tunnel is intended for experimental testing of models in a controlled airflow environment and its design offers an affordable and practical solution for researchers and stud...
Published in: | JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION |
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Main Authors: | , , , , , , |
Format: | Article |
Language: | English |
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AERONAUTICAL & ASTRONAUTICAL SOC REPUBLIC CHINA
2024
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Online Access: | https://www-webofscience-com.uitm.idm.oclc.org/wos/woscc/full-record/WOS:001278414200001 |
author |
Marzuki Omar Faruqi; Alik Muhammad Aliff Najmi; Teo Ellie Yi Lih; Rafie Azmin Shakrine Mohd; Pendek Zainol Ariffin; Adam Nor Mariah |
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Marzuki Omar Faruqi; Alik Muhammad Aliff Najmi; Teo Ellie Yi Lih; Rafie Azmin Shakrine Mohd; Pendek Zainol Ariffin; Adam Nor Mariah Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser Engineering |
author_facet |
Marzuki Omar Faruqi; Alik Muhammad Aliff Najmi; Teo Ellie Yi Lih; Rafie Azmin Shakrine Mohd; Pendek Zainol Ariffin; Adam Nor Mariah |
author_sort |
Marzuki |
spelling |
Marzuki, Omar Faruqi; Alik, Muhammad Aliff Najmi; Teo, Ellie Yi Lih; Rafie, Azmin Shakrine Mohd; Pendek, Zainol Ariffin; Adam, Nor Mariah Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION English Article This paper presents the design and construction of a small open jet wind tunnel without the contraction and diffuser. The wind tunnel is intended for experimental testing of models in a controlled airflow environment and its design offers an affordable and practical solution for researchers and students to conduct their aerodynamic experiments on small-scale models. The paper outlines key considerations for designing and constructing the wind tunnel, including selected blower fan and design of the fan holder structure. The wind tunnel is successfully constructed and tested, and the results have shown that the airflow with an average of 4 m/s and turbulence intensity of 15%. Through its capacity to provide a wide range of turbulence intensities (i.e. 15% - 89%), this wind tunnel empowers researchers to explore an extensive spectrum of real -world conditions, ensuring that the experimental data more authentically mirrors the dynamic characteristics of outdoor environments. This enhanced versatility in turbulence intensity is of particular importance, especially given the marked variations in turbulence levels that have been evident across the different urban locales. Consequently, this study not only furnishes the practical guidance for constructing small open jet wind tunnels but also highlights the critical significance of regulating turbulence intensity, varying between 89% at a distance of 200 mm and 15% at 2000 mm from the outlet to ensure precise experimental fidelity. AERONAUTICAL & ASTRONAUTICAL SOC REPUBLIC CHINA 1990-7710 2024 56 1 10.6125/JoAAA.202403_56(1S).09 Engineering WOS:001278414200001 https://www-webofscience-com.uitm.idm.oclc.org/wos/woscc/full-record/WOS:001278414200001 |
title |
Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser |
title_short |
Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser |
title_full |
Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser |
title_fullStr |
Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser |
title_full_unstemmed |
Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser |
title_sort |
Design and Construction of a Small Open-air Wind Tunnel without Contraction and Diffuser |
container_title |
JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION |
language |
English |
format |
Article |
description |
This paper presents the design and construction of a small open jet wind tunnel without the contraction and diffuser. The wind tunnel is intended for experimental testing of models in a controlled airflow environment and its design offers an affordable and practical solution for researchers and students to conduct their aerodynamic experiments on small-scale models. The paper outlines key considerations for designing and constructing the wind tunnel, including selected blower fan and design of the fan holder structure. The wind tunnel is successfully constructed and tested, and the results have shown that the airflow with an average of 4 m/s and turbulence intensity of 15%. Through its capacity to provide a wide range of turbulence intensities (i.e. 15% - 89%), this wind tunnel empowers researchers to explore an extensive spectrum of real -world conditions, ensuring that the experimental data more authentically mirrors the dynamic characteristics of outdoor environments. This enhanced versatility in turbulence intensity is of particular importance, especially given the marked variations in turbulence levels that have been evident across the different urban locales. Consequently, this study not only furnishes the practical guidance for constructing small open jet wind tunnels but also highlights the critical significance of regulating turbulence intensity, varying between 89% at a distance of 200 mm and 15% at 2000 mm from the outlet to ensure precise experimental fidelity. |
publisher |
AERONAUTICAL & ASTRONAUTICAL SOC REPUBLIC CHINA |
issn |
1990-7710 |
publishDate |
2024 |
container_volume |
56 |
container_issue |
1 |
doi_str_mv |
10.6125/JoAAA.202403_56(1S).09 |
topic |
Engineering |
topic_facet |
Engineering |
accesstype |
|
id |
WOS:001278414200001 |
url |
https://www-webofscience-com.uitm.idm.oclc.org/wos/woscc/full-record/WOS:001278414200001 |
record_format |
wos |
collection |
Web of Science (WoS) |
_version_ |
1809679297876590592 |