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...
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Veröffentlicht in: | Journal of propulsion and power 2013-11, Vol.29 (6), p.1374-1381 |
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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 |
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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. 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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. 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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. 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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> |
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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 |
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