Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/5972
Title: Simulation of suppression of vortex breakdown over delta wings by vortex filament method
Authors: Lewpiriyawong Nuttawut.
Keywords: DRNTU::Engineering::Aeronautical engineering
Issue Date: 2006
Source: Lewpiriyawong, N. (2006). Simulation of suppression of vortex breakdown over delta wings by vortex filament method. Master’s thesis, Nanyang Technological University, Singapore.
Abstract: This study focuses on three-dimensional evolution of unperturbed and perturbed leading-edge vortices over delta wings. Since the vortex filament method can discretize the high vorticity-containing region of vorticity fields and track this discretization in a Lagrangian frame, it is chosen to simulate the core of the leading-edge vortices. The purpose of perturbing the vortex core is to delay or suppress vortex breakdown over delta wings.
URI: http://hdl.handle.net/10356/5972
Rights: Nanyang Technological University
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Theses

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