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

• Main Authors: UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin
• Format: Conference or Workshop Item
• 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/58741/1/58741_Comparison%20of%20data%20correction%20methods_complete.pdf; http://irep.iium.edu.my/58741/2/58741_Comparison%20of%20data%20correction%20methods_scopus.pdf; http://irep.iium.edu.my/58741/; https://www.epj-conferences.org/articles/epjconf/abs/2016/09/epjconf_efm2016_02129/epjconf_efm2016_02129.html
• Institution: Universiti Islam Antarabangsa Malaysia

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...