Optimization of maximum lift to drag ratio on airfoil design based on Artificial Neural Network utilizing Genetic Algorithm

SINAGA , Nazaruddin Optimization of maximum lift to drag ratio on airfoil design based on Artificial Neural Network utilizing Genetic Algorithm. UNDIP.

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Item Type:Other
Subjects:T Technology > TJ Mechanical engineering and machinery
Divisions:Faculty of Engineering > Department of Mechanical Engineering
Faculty of Engineering > Department of Mechanical Engineering
ID Code:79661
Deposited By:Dwinita Fibriani
Deposited On:21 Jan 2020 12:52
Last Modified:21 Jan 2020 12:52

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