Prediction of aerodynamic characteristics of an aircraft model with and without winglet using fuzzy logic technique
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...
Main Authors: | Hossain, A., Rahman, A., Hossen, J., Iqbal, A.K.M.P., Zahirul, M.I. |
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Published: |
2017
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Online Access: | http://dspace.uniten.edu.my/jspui/handle/123456789/6317 |
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