Fuzzy logic approach for prediction the lift coefficient on an aircraft model with and without winglet

Fuzzy logic approach for prediction the lift coefficient on an aircraft model with and without winglet

This paper describes the unique structure of an aircraft model with and without winglet tested at Aerodynamics Laboratory, Faculty of Engineering (University Putra Malaysia) using subsonic wind tunnel of 1000 mm × 1000 mm rectangular test section and 2500 mm long. Focusing on predicting the aerodyna...

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Bibliographic Details
Main Authors: Hossain, Altab, Rahman, Mohammed Ataur, Mohiuddin, A. K. M., Iqbal, Parvez, Muhidin, Arifin, Mohamad, Mazian
Format: Conference or Workshop Item
Language:English
Published: 2009
Subjects:
T Technology (General)
TJ Mechanical engineering and machinery
Online Access:http://irep.iium.edu.my/1494/
http://irep.iium.edu.my/1494/1/ICME_2009-FM18.pdf

Internet

http://irep.iium.edu.my/1494/
http://irep.iium.edu.my/1494/1/ICME_2009-FM18.pdf

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