Investigations on symmetric and asymmetric NACA airfoils with different thickness ratios flow and acoustic characteristics

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dc.contributor.authorKumar, Sujit
dc.date.accessioned2023-03-09T05:34:23Z
dc.date.available2023-03-09T05:34:23Z
dc.date.issued2023-02
dc.identifier.urihttp://hdl.handle.net/123456789/2705
dc.language.isoenen_US
dc.publisherIndian Institute of Technology (Indian School of Mines) Dhanbaden_US
dc.subjectAerodynamicsen_US
dc.subjectSymmetric NACA airfoilsen_US
dc.subjectasymmetric NACA airfoilsen_US
dc.subjectthickness ratiosen_US
dc.subjectlaminar separation bubbleen_US
dc.subjectpressure coefficienten_US
dc.subjectPh.Den_US
dc.subjectMECHen_US
dc.subjectPH2400en_US
dc.titleInvestigations on symmetric and asymmetric NACA airfoils with different thickness ratios flow and acoustic characteristicsen_US
dc.typeThesisen_US
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