Low-Order Computational Modeling of Propeller-Wing Aerodynamic Interaction Using Wake Vortex Decomposition and Weissinger Method.

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dc.contributor.advisorAshok Gopalarathnam, Chair
dc.contributor.advisorKenneth Granlund, Member
dc.contributor.advisorMatthew Bryant, Member
dc.contributor.authorRao, Neel
dc.date.accepted2024-11-15
dc.date.accessioned2025-05-15T12:30:36Z
dc.date.available2025-05-15T12:30:36Z
dc.date.defense2024-10-25
dc.date.embargo2025-05-15
dc.date.issued2024-10-25
dc.date.released2025-05-15
dc.date.reviewed2024-10-31
dc.date.submitted2024-10-28
dc.degree.disciplineAerospace Engineering
dc.degree.levelthesis
dc.degree.nameMaster of Science
dc.identifier.otherdeg39803
dc.identifier.urihttps://www.lib.ncsu.edu/resolver/1840.20/45360
dc.titleLow-Order Computational Modeling of Propeller-Wing Aerodynamic Interaction Using Wake Vortex Decomposition and Weissinger Method.

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