Prediction of aerodynamic characteristics of an aircraft model with and without winglet using fuzzy logic technique

• Main Authors: Hossain, Altab, Rahman, Mohammed Ataur, Hossen, Jakir, Iqbal, Parvez, M.I., Zahirul
• Format: Article
• Language: English
• Published: Elsevier 2011
• Subjects: TL500 Aeronautics
• Online Access: http://irep.iium.edu.my/7597/1/Journal_of_Aerospace_Science_and_Technology_%28ISI%29_Listed_%5B15%282011%29%5D.pdf; http://irep.iium.edu.my/7597/; http://www.sciencedirect.com/science/article/pii/S1270963810001586
• Institution: Universiti Islam Antarabangsa Malaysia

This paper describes the potentials of an aircraft model without and with winglet attached with NACA wing No. 65-3-218. Based on the longitudinal aerodynamic characteristics analyzing for the aircraft model tested in low subsonic wind tunnel, the lift coefficient (CL ) and drag coefficient (CD) were...