Development of Delta Wing Aerodynamics Research in Universiti Teknologi Malaysia Low Speed Wind Tunnel

Development of Delta Wing Aerodynamics Research in Universiti Teknologi Malaysia Low Speed Wind Tunnel

This paper presents wind tunnel experiment on two delta wing configurations which are differentiated by their leading edge profiles: sharp and round-edged wings. The experiments were performed as a part of the delta wing aerodynamics research development in Universiti Teknologi Malaysia, low speed t...

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Bibliographic Details
Main Authors: Shabudin Mat, I. S. Ishak, Tholudin Mat Lazim, Shuhaimi Mansor, Mazuriah Said, Abdul Basid Abdul Rahman, Ahmad Shukeri Mohd. Kamaludim, Romain Brossay
Format: Article
Language:English
Published: SAGE Publishing 2014-07-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1155/2014/434892

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