Comparison of data correction methods for blockage effects in semispan wing model testing

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Comparison of data correction methods for blockage effects in semispan wing model testing

Wing alone models are usually tested in wind tunnels for aerospace applications like aircraft and hybrid buoyant aircraft. Raw data obtained from such testing is subject to different corrections such as wall interference, blockage, offset in angle of attack, dynamic pressure and free stream velocity...

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Bibliographic Details
Main Authors:	UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin
Format:	Proceeding Paper
Language:	English English
Published:	EDP Sciences 2016
Subjects:	TK7800 Electronics. Computer engineering. Computer hardware. Photoelectronic devices TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/58741/ http://irep.iium.edu.my/58741/1/58741_Comparison%20of%20data%20correction%20methods_complete.pdf http://irep.iium.edu.my/58741/2/58741_Comparison%20of%20data%20correction%20methods_scopus.pdf

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