Optimization Of Maximum Lift ToDrag Ratio On Airfoil Design

Based On Artificial NeuralNetwork Utilizing Genetic

Algorithmby Nazaruddin Sinaga

Submission date: 13-Jan-2020 10:24AM (UTC+0700)Submission ID: 1241281252File name: 5.pdf (4.11M)Word count: 2277Character count: 11239

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Optimization Of Maximum Lift To Drag Ratio On Airfoil DesignBased On Artificial Neural Network Utilizing Genetic AlgorithmORIGINALITY REPORT

PRIMARY SOURCES

www.siam.orgInternet Source

Ernst Heinrich Hirschel. "AerothermodynamicDesign Problems of Non-Winged Re-EntryVehicles", Selected Aerothermodynamic DesignProblems of Hypersonic Flight Vehicles, 2009Publication

www.eurasphalt.orgInternet Source

FINAL GRADE

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Optimization Of Maximum Lift To Drag Ratio On Airfoil DesignBased On Artificial Neural Network Utilizing Genetic AlgorithmGRADEMARK REPORT

GENERAL COMMENTS

Instructor

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