Aerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation.

Show full item record

Title: Aerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation.
Author: Thompson, Kyle Bonner
Advisors: Hassan Hassan, Co-Chair
Peter Gnoffo, Co-Chair
Jack Edwards, Member
John Griggs, Graduate School Representative
Hong Luo, Member
Date: 2017-03-17
Degree: Doctor of Philosophy
Discipline: Aerospace Engineering
URI: http://www.lib.ncsu.edu/resolver/1840.20/33558


Files in this item

Files Size Format View
etd.pdf 1.579Mb PDF View/Open

This item appears in the following Collection(s)

Show full item record