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University of Illinois at Urbana-Champaign
A numerical study of hypersonic flows using the full Navier-Stokes equations with different air models
Abstract
dc:descriptionA two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and nonequilibrium air models. The effects of a real gas are investigated numerically in the hypersonic flow regime.
Degree
thesis:*- Name thesis:degree_name
- Ph.D.
- Level thesis:degree_level
- Dissertation
- Discipline thesis:degree_discipline
- Aeronautical and Astronautical Engineering
- Grantor
- University of Illinois at Urbana-Champaign
- Year dc:date
- 2011
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Kim, Moon-Sang
- Contributors dc:contributor
-
- Lee, Ki D.
Subjects
dc:subject × 1Rights
dc:rights- Statement dc:rights
-
- Copyright 1991 Kim, Moon-Sang
- Language dc:language
- eng
Identifiers
dc:identifier.*- Identifier
-
AAI9210867
(UMI)AAI9210867 - OAI identifier oai:identifier
- oai:www.ideals.illinois.edu:2142/19155