Optimization Of Maximum Lift To Drag Ratio On Airfoil Design Based On Artificial Neural Network Utilizing Genetic Algorithm by Nazaruddin Sinaga Submission date: 13-Jan-2020 10:24AM (UTC+0700) Submission ID: 1241281252 File name: 5.pdf (4.11M) Word count: 2277 Character count: 11239
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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
6%SIMILARITY INDEX
5%INTERNET SOURCES
5%PUBLICATIONS
0%STUDENT PAPERS
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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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