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University of Illinois at Urbana-Champaign
Direct simulation of the fluid-structure interaction of a compliant panel in a hypersonic compression ramp flow
Abstract
dc:descriptionMade available in DSpace on 2019-08-23T20:05:24Z (GMT). No. of bitstreams: 2 SULLIVAN-THESIS-2019.pdf: 17201247 bytes, checksum: d0a3b3cb0abcb1c32abeaa87d376612e (MD5) LICENSE.txt: 4212 bytes, checksum: 6e46c83f39344ca0c821874c7c9c44e6 (MD5) Previous issue date: 2019-04-26
Degree
thesis:*- Name thesis:degree_name
- M.S.
- Level thesis:degree_level
- Thesis
- Discipline thesis:degree_discipline
- Aerospace Engineering
- Grantor
- University of Illinois at Urbana-Champaign
- Year dc:date
- 2019
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Sullivan, Bryson
- Contributors dc:contributor
-
- Bodony, Daniel J.
Subjects
dc:subject × 1Rights
dc:rights- Statement dc:rights
-
- Copyright 2019 Bryson Sullivan
- Language dc:language
- en
Identifiers
dc:identifier.*- Handle dc:identifier
- http://hdl.handle.net/2142/104947
- OAI identifier oai:identifier
- oai:www.ideals.illinois.edu:2142/104947