Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05

Hale, Jason

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University of Illinois at Urbana-Champaign

Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05

dc:creator Hale, Jason

thesis:degree_name M.S.

dc:date2015

Abstract

dc:description

U of I Only Restriction Lifted for Item 73181 on 2017-01-22T10:15:29Z.

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: 2015

Author and committee

dc:creator, dc:contributor.*

Author dc:creator: Hale, Jason
Contributors dc:contributor: Elliott, Gregory S.
Dutton, J.C.

Subjects

dc:subject × 7

Rights

dc:rights

Language dc:language: en

Identifiers

dc:identifier.*

Handle dc:identifier: http://hdl.handle.net/2142/72992
OAI identifier oai:identifier: oai:www.ideals.illinois.edu:2142/72992

Chain of custody

source

Harvested from: University of Illinois - Urbana-Champaign
Base URL: www.ideals.illinois.edu/oai-pmh
Last updated: 2026-07-22
Source record: OAI-PMH GetRecord

related terms

citation

Hale, Jason. Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05. Thesis thesis, University of Illinois at Urbana-Champaign, 2015. http://hdl.handle.net/2142/72992

Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05

Abstract

Degree

Author and committee

Subjects

Rights

Identifiers

Chain of custody

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