Optimization of Maximum Lift to Drag Ratio on Airfoil Design
Based on Artificial Neural Network Utilizing Genetic
Algorithm
by Ismoyo Haryanto
Submission date: 08-May-2020 11:03AM (UTC+0700) Submission ID: 1319121241
File name: Optimization_Of_Maximum_Lift_To_Drag_Ratio_On_Airf.pdf (473.57K) Word count: 2958
Character count: 15015
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Optimization of Maximum Lift to Drag Ratio on Airfoil Design Based on Artificial Neural Network Utilizing Genetic Algorithm
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Munadi, M. Amirullah Akbar. "Simulation of fuzzy logic control for DC servo motor using Arduino based on MATLAB/Simulink", 2014 International Conference on Intelligent
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J L Cuerno-Rejado. "Experimental aerodynamic characteristics of NACA 0012 airfoils with
simulated glaze and rime ice", Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 01/01/2001
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Hamid Ahmadi Asl, Reza Kamali Monfared,
Manouchehr Rad. "Experimental investigation of blade number and design effects for a ducted wind turbine", Renewable Energy, 2017
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Karthikeyan, N., K. Kalidasa Murugavel, S. Arun Kumar, and S. Rajakumar. "Review of
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Sustainable Energy Reviews, 2015.
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Optimization of Maximum Lift to Drag Ratio on Airfoil Design Based on Artificial Neural Network Utilizing Genetic Algorithm
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