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...

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Published in:JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION
Main Authors: Marzuki, Omar Faruqi; Alik, Muhammad Aliff Najmi; Teo, Ellie Yi Lih; Rafie, Azmin Shakrine Mohd; Pendek, Zainol Ariffin; Adam, Nor Mariah
Format: Article
Language:English
Published: AERONAUTICAL & ASTRONAUTICAL SOC REPUBLIC CHINA 2024
Subjects:
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
spellingShingle 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
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