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: Mat, Shabudin, Ishak, Irny Suzila, Mat Lazim, Tholudin, Mansor, Shuhaimi, Said, Mazuriah, Abd. Rahman, Abdul Basid, Mohd. Kamaludim, Ahmad Shukeri, Brossay, Romain
Format: Article
Language:English
Published: Hindawi Publishing Corporation 2014
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Online Access:http://eprints.utm.my/id/eprint/52368/1/ShabudinMat2014_Developmentofdeltawing.pdf
http://eprints.utm.my/id/eprint/52368/
http://dx.doi.org/10.1155/2014/434892
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