An Inviscid Numerical Method for Unsteady Flows Over Airfoils and Wings to Predict the Onset of Leading Edge Vortex Formation.

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dc.contributor.advisorAshok Gopalarathnam, Chairen_US
dc.contributor.advisorJack Edwards, Memberen_US
dc.contributor.advisorAndre Mazzoleni, Memberen_US
dc.contributor.authorAggarwal, Sachinen_US
dc.date.accepted2013-11-27en_US
dc.date.accessioned2013-11-28T10:30:07Z
dc.date.available2013-11-28T10:30:07Z
dc.date.defense2013-10-25en_US
dc.date.issued2013-10-25en_US
dc.date.released2013-11-28en_US
dc.date.reviewed2013-10-30en_US
dc.date.submitted2013-10-25en_US
dc.degree.disciplineAerospace Engineeringen_US
dc.degree.levelthesisen_US
dc.degree.nameMaster of Scienceen_US
dc.identifier.otherdeg3013en_US
dc.identifier.urihttp://www.lib.ncsu.edu/resolver/1840.16/9084
dc.rightsen_US
dc.titleAn Inviscid Numerical Method for Unsteady Flows Over Airfoils and Wings to Predict the Onset of Leading Edge Vortex Formation.en_US

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