A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact
The effects of shock wave impact on unsteady turbine heat transfer are investigated. A numerical approach is developed to simulate the flow physics present in a previously performed unsteady wind tunnel experiment. The windtunnel experiment included unheated and heated flows over a cascade of highl...
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ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-259832020-09-29T05:31:39Z A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact Reid, Terry Vincent Mechanical Engineering Ng, Fai Scott, Elaine P. Nelson, Douglas J. Diller, Thomas E. Schetz, Joseph A. Unsteady computations heat flux The effects of shock wave impact on unsteady turbine heat transfer are investigated. A numerical approach is developed to simulate the flow physics present in a previously performed unsteady wind tunnel experiment. The windtunnel experiment included unheated and heated flows over a cascade of highly loaded turbine blades. After the flow over the blades was established, a single shock with a pressure ratio of 1.1 was introduced into the wind tunnel test section. A single blade was equipped with pressure transducers and heat flux microsensors. As the shock wave strikes the blade, time resolved pressure, temperature, and heat transfer data were recorded. Ph. D. 2014-03-14T20:06:41Z 2014-03-14T20:06:41Z 1998-04-30 1999-01-10 1999-02-05 1999-02-05 Dissertation etd-011099-132537 http://hdl.handle.net/10919/25983 http://scholar.lib.vt.edu/theses/available/etd-011099-132537/ Chapt5.pdf Chapt4.pdf Chapt7.pdf Back.pdf Chapt6.pdf Chapt3.pdf Front.pdf Chapt2.pdf Chapt1.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf Virginia Tech |
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Unsteady computations heat flux |
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Unsteady computations heat flux Reid, Terry Vincent A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact |
description |
The effects of shock wave impact on unsteady turbine heat transfer are investigated. A numerical approach is developed to simulate the flow physics present in a previously performed unsteady wind tunnel experiment.
The windtunnel experiment included unheated and heated flows over a cascade of highly loaded turbine blades. After the flow over the blades was established, a single shock with a pressure ratio of 1.1 was introduced into the wind tunnel test section. A single blade was equipped with pressure transducers and heat flux microsensors. As the shock wave strikes the blade, time resolved pressure, temperature, and heat transfer data were recorded. === Ph. D. |
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Mechanical Engineering |
author_facet |
Mechanical Engineering Reid, Terry Vincent |
author |
Reid, Terry Vincent |
author_sort |
Reid, Terry Vincent |
title |
A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact |
title_short |
A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact |
title_full |
A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact |
title_fullStr |
A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact |
title_full_unstemmed |
A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact |
title_sort |
computational approach for investigating unsteady turbine heat transfer due to shock wave impact |
publisher |
Virginia Tech |
publishDate |
2014 |
url |
http://hdl.handle.net/10919/25983 http://scholar.lib.vt.edu/theses/available/etd-011099-132537/ |
work_keys_str_mv |
AT reidterryvincent acomputationalapproachforinvestigatingunsteadyturbineheattransferduetoshockwaveimpact AT reidterryvincent computationalapproachforinvestigatingunsteadyturbineheattransferduetoshockwaveimpact |
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