Adaptive Mesh Euler Equation Computations of Vortex Breakdown in Delta Wing Flow

Adaptive Mesh Euler Equation Computations of Vortex Breakdown in Delta Wing Flow

A solution method for the three-dimensional Euler equations is formulated and implemented. The solver uses an unstructured mesh of tetrahedral cells and performs adaptive refinement by mesh-point embedding to increase mesh resolution in regions of interesting flow features. The fourth-difference...

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Bibliographic Details
Main Author:	Modiano, David
Format:	Technical Report
Language:	en_US
Published:	Aerospace Computational Design Lab, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology 2012
Online Access:	http://hdl.handle.net/1721.1/70577

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