Effect of Cooling Injection on Transonic Tip Flows

In this paper, the effect of cooling injection on the aerodynamics of tip flows in transonic turbines is investigated. Experiments are performed using an idealized model of a transonic tip flow. Schlieren photography, probe, and surface pressure measurements are used to determine the transonic tip f...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of propulsion and power 2013-11, Vol.29 (6), p.1374-1381
Hauptverfasser: Wheeler, Andrew P. S, Saleh, Zainab
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 1381
container_issue 6
container_start_page 1374
container_title Journal of propulsion and power
container_volume 29
creator Wheeler, Andrew P. S
Saleh, Zainab
description In this paper, the effect of cooling injection on the aerodynamics of tip flows in transonic turbines is investigated. Experiments are performed using an idealized model of a transonic tip flow. Schlieren photography, probe, and surface pressure measurements are used to determine the transonic tip flow structure and to validate the computational method. Computational simulations are performed to investigate the effects of cooling injection in a transonic blade environment. The results show that cooling injection has the potential to reduce overtip leakage loss.
doi_str_mv 10.2514/1.B34657
format Article
fullrecord <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_proquest_miscellaneous_1762140089</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3111539361</sourcerecordid><originalsourceid>FETCH-LOGICAL-a418t-b73a1eefb15a4d56e36f28bd94842d8b4b7afd1978a5c9c68a6745c32ddbb7a03</originalsourceid><addsrcrecordid>eNqFkU9LAzEQxYMoWKvgR1gQwctqJpn82aOWVgsFL_UcsruJpGw3ddMifnsj9VB6UBgYePPjDTOPkGug90wAPsD9E0cp1AkZgeC85FrJUzKiCnWZdX1OLlJaUQpSSzUibOq9a7ZF9MUkxi7078W8X2UlxL7ItRxsn2IfmmIZNsWsi5_pkpx52yV39dvH5G02XU5eysXr83zyuCgtgt6WteIWnPM1CIutkI5Lz3TdVqiRtbrGWlnfQqW0FU3VSG2lQtFw1rZ1HlE-Jnd7380QP3Yubc06pMZ1ne1d3CUDSjJASnX1P4oShZBAVUZvjtBV3A19PsQwrLikiIz-RQHmNzKu8WBtM8SUBufNZghrO3wZoOYnDQNmn0ZGb_eoDdYemB1z3007g-8</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1446523849</pqid></control><display><type>article</type><title>Effect of Cooling Injection on Transonic Tip Flows</title><source>Alma/SFX Local Collection</source><creator>Wheeler, Andrew P. S ; Saleh, Zainab</creator><creatorcontrib>Wheeler, Andrew P. S ; Saleh, Zainab</creatorcontrib><description>In this paper, the effect of cooling injection on the aerodynamics of tip flows in transonic turbines is investigated. Experiments are performed using an idealized model of a transonic tip flow. Schlieren photography, probe, and surface pressure measurements are used to determine the transonic tip flow structure and to validate the computational method. Computational simulations are performed to investigate the effects of cooling injection in a transonic blade environment. The results show that cooling injection has the potential to reduce overtip leakage loss.</description><identifier>ISSN: 0748-4658</identifier><identifier>EISSN: 1533-3876</identifier><identifier>DOI: 10.2514/1.B34657</identifier><identifier>CODEN: JPPOEL</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Computation ; Computer simulation ; Cooling ; Cooling effects ; Leakage ; Pressure ; Schlieren photography ; Surface pressure ; Transonic flow ; Turbines</subject><ispartof>Journal of propulsion and power, 2013-11, Vol.29 (6), p.1374-1381</ispartof><rights>Copyright © 2013 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code and $10.00 in correspondence with the CCC.</rights><rights>Copyright © 2013 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code 1533-3876/13 and $10.00 in correspondence with the CCC.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a418t-b73a1eefb15a4d56e36f28bd94842d8b4b7afd1978a5c9c68a6745c32ddbb7a03</citedby><cites>FETCH-LOGICAL-a418t-b73a1eefb15a4d56e36f28bd94842d8b4b7afd1978a5c9c68a6745c32ddbb7a03</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Wheeler, Andrew P. S</creatorcontrib><creatorcontrib>Saleh, Zainab</creatorcontrib><title>Effect of Cooling Injection on Transonic Tip Flows</title><title>Journal of propulsion and power</title><description>In this paper, the effect of cooling injection on the aerodynamics of tip flows in transonic turbines is investigated. Experiments are performed using an idealized model of a transonic tip flow. Schlieren photography, probe, and surface pressure measurements are used to determine the transonic tip flow structure and to validate the computational method. Computational simulations are performed to investigate the effects of cooling injection in a transonic blade environment. The results show that cooling injection has the potential to reduce overtip leakage loss.</description><subject>Computation</subject><subject>Computer simulation</subject><subject>Cooling</subject><subject>Cooling effects</subject><subject>Leakage</subject><subject>Pressure</subject><subject>Schlieren photography</subject><subject>Surface pressure</subject><subject>Transonic flow</subject><subject>Turbines</subject><issn>0748-4658</issn><issn>1533-3876</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><recordid>eNqFkU9LAzEQxYMoWKvgR1gQwctqJpn82aOWVgsFL_UcsruJpGw3ddMifnsj9VB6UBgYePPjDTOPkGug90wAPsD9E0cp1AkZgeC85FrJUzKiCnWZdX1OLlJaUQpSSzUibOq9a7ZF9MUkxi7078W8X2UlxL7ItRxsn2IfmmIZNsWsi5_pkpx52yV39dvH5G02XU5eysXr83zyuCgtgt6WteIWnPM1CIutkI5Lz3TdVqiRtbrGWlnfQqW0FU3VSG2lQtFw1rZ1HlE-Jnd7380QP3Yubc06pMZ1ne1d3CUDSjJASnX1P4oShZBAVUZvjtBV3A19PsQwrLikiIz-RQHmNzKu8WBtM8SUBufNZghrO3wZoOYnDQNmn0ZGb_eoDdYemB1z3007g-8</recordid><startdate>20131101</startdate><enddate>20131101</enddate><creator>Wheeler, Andrew P. S</creator><creator>Saleh, Zainab</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20131101</creationdate><title>Effect of Cooling Injection on Transonic Tip Flows</title><author>Wheeler, Andrew P. S ; Saleh, Zainab</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a418t-b73a1eefb15a4d56e36f28bd94842d8b4b7afd1978a5c9c68a6745c32ddbb7a03</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Computation</topic><topic>Computer simulation</topic><topic>Cooling</topic><topic>Cooling effects</topic><topic>Leakage</topic><topic>Pressure</topic><topic>Schlieren photography</topic><topic>Surface pressure</topic><topic>Transonic flow</topic><topic>Turbines</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wheeler, Andrew P. S</creatorcontrib><creatorcontrib>Saleh, Zainab</creatorcontrib><collection>CrossRef</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of propulsion and power</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wheeler, Andrew P. S</au><au>Saleh, Zainab</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Effect of Cooling Injection on Transonic Tip Flows</atitle><jtitle>Journal of propulsion and power</jtitle><date>2013-11-01</date><risdate>2013</risdate><volume>29</volume><issue>6</issue><spage>1374</spage><epage>1381</epage><pages>1374-1381</pages><issn>0748-4658</issn><eissn>1533-3876</eissn><coden>JPPOEL</coden><abstract>In this paper, the effect of cooling injection on the aerodynamics of tip flows in transonic turbines is investigated. Experiments are performed using an idealized model of a transonic tip flow. Schlieren photography, probe, and surface pressure measurements are used to determine the transonic tip flow structure and to validate the computational method. Computational simulations are performed to investigate the effects of cooling injection in a transonic blade environment. The results show that cooling injection has the potential to reduce overtip leakage loss.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.B34657</doi><tpages>8</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0748-4658
ispartof Journal of propulsion and power, 2013-11, Vol.29 (6), p.1374-1381
issn 0748-4658
1533-3876
language eng
recordid cdi_proquest_miscellaneous_1762140089
source Alma/SFX Local Collection
subjects Computation
Computer simulation
Cooling
Cooling effects
Leakage
Pressure
Schlieren photography
Surface pressure
Transonic flow
Turbines
title Effect of Cooling Injection on Transonic Tip Flows
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T20%3A58%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_aiaa_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Effect%20of%20Cooling%20Injection%20on%20Transonic%20Tip%20Flows&rft.jtitle=Journal%20of%20propulsion%20and%20power&rft.au=Wheeler,%20Andrew%20P.%20S&rft.date=2013-11-01&rft.volume=29&rft.issue=6&rft.spage=1374&rft.epage=1381&rft.pages=1374-1381&rft.issn=0748-4658&rft.eissn=1533-3876&rft.coden=JPPOEL&rft_id=info:doi/10.2514/1.B34657&rft_dat=%3Cproquest_aiaa_%3E3111539361%3C/proquest_aiaa_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1446523849&rft_id=info:pmid/&rfr_iscdi=true