Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system
Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with...
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| Autor*in: |
Seo, Heerim [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2022 |
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| Anmerkung: |
© The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
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| Übergeordnetes Werk: |
Enthalten in: Journal of visualization - Berlin : Springer, 1998, 26(2022), 1 vom: 30. Aug., Seite 61-81 |
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| Übergeordnetes Werk: |
volume:26 ; year:2022 ; number:1 ; day:30 ; month:08 ; pages:61-81 |
| Links: |
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| DOI / URN: |
10.1007/s12650-022-00869-0 |
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| Katalog-ID: |
SPR049203290 |
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| 245 | 1 | 0 | |a Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system |
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| 520 | |a Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract | ||
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| 700 | 1 | |a Kwon, Daehee |4 aut | |
| 700 | 1 | |a Lee, Seungju |4 aut | |
| 700 | 1 | |a Yeom, Eunseop |0 (orcid)0000-0002-9717-030X |4 aut | |
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10.1007/s12650-022-00869-0 doi (DE-627)SPR049203290 (SPR)s12650-022-00869-0-e DE-627 ger DE-627 rakwb eng Seo, Heerim verfasserin aut Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract Jet Impingement (dpeaa)DE-He213 Effusion Holes (dpeaa)DE-He213 Wall Jet (dpeaa)DE-He213 Concave Surface (dpeaa)DE-He213 PIV (dpeaa)DE-He213 CFD (dpeaa)DE-He213 Turbulence Model (dpeaa)DE-He213 Kwon, Daehee aut Lee, Seungju aut Yeom, Eunseop (orcid)0000-0002-9717-030X aut Enthalten in Journal of visualization Berlin : Springer, 1998 26(2022), 1 vom: 30. Aug., Seite 61-81 (DE-627)357174291 (DE-600)2094841-4 1875-8975 nnns volume:26 year:2022 number:1 day:30 month:08 pages:61-81 https://dx.doi.org/10.1007/s12650-022-00869-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 26 2022 1 30 08 61-81 |
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10.1007/s12650-022-00869-0 doi (DE-627)SPR049203290 (SPR)s12650-022-00869-0-e DE-627 ger DE-627 rakwb eng Seo, Heerim verfasserin aut Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract Jet Impingement (dpeaa)DE-He213 Effusion Holes (dpeaa)DE-He213 Wall Jet (dpeaa)DE-He213 Concave Surface (dpeaa)DE-He213 PIV (dpeaa)DE-He213 CFD (dpeaa)DE-He213 Turbulence Model (dpeaa)DE-He213 Kwon, Daehee aut Lee, Seungju aut Yeom, Eunseop (orcid)0000-0002-9717-030X aut Enthalten in Journal of visualization Berlin : Springer, 1998 26(2022), 1 vom: 30. Aug., Seite 61-81 (DE-627)357174291 (DE-600)2094841-4 1875-8975 nnns volume:26 year:2022 number:1 day:30 month:08 pages:61-81 https://dx.doi.org/10.1007/s12650-022-00869-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 26 2022 1 30 08 61-81 |
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10.1007/s12650-022-00869-0 doi (DE-627)SPR049203290 (SPR)s12650-022-00869-0-e DE-627 ger DE-627 rakwb eng Seo, Heerim verfasserin aut Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract Jet Impingement (dpeaa)DE-He213 Effusion Holes (dpeaa)DE-He213 Wall Jet (dpeaa)DE-He213 Concave Surface (dpeaa)DE-He213 PIV (dpeaa)DE-He213 CFD (dpeaa)DE-He213 Turbulence Model (dpeaa)DE-He213 Kwon, Daehee aut Lee, Seungju aut Yeom, Eunseop (orcid)0000-0002-9717-030X aut Enthalten in Journal of visualization Berlin : Springer, 1998 26(2022), 1 vom: 30. Aug., Seite 61-81 (DE-627)357174291 (DE-600)2094841-4 1875-8975 nnns volume:26 year:2022 number:1 day:30 month:08 pages:61-81 https://dx.doi.org/10.1007/s12650-022-00869-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 26 2022 1 30 08 61-81 |
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10.1007/s12650-022-00869-0 doi (DE-627)SPR049203290 (SPR)s12650-022-00869-0-e DE-627 ger DE-627 rakwb eng Seo, Heerim verfasserin aut Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract Jet Impingement (dpeaa)DE-He213 Effusion Holes (dpeaa)DE-He213 Wall Jet (dpeaa)DE-He213 Concave Surface (dpeaa)DE-He213 PIV (dpeaa)DE-He213 CFD (dpeaa)DE-He213 Turbulence Model (dpeaa)DE-He213 Kwon, Daehee aut Lee, Seungju aut Yeom, Eunseop (orcid)0000-0002-9717-030X aut Enthalten in Journal of visualization Berlin : Springer, 1998 26(2022), 1 vom: 30. Aug., Seite 61-81 (DE-627)357174291 (DE-600)2094841-4 1875-8975 nnns volume:26 year:2022 number:1 day:30 month:08 pages:61-81 https://dx.doi.org/10.1007/s12650-022-00869-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 26 2022 1 30 08 61-81 |
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10.1007/s12650-022-00869-0 doi (DE-627)SPR049203290 (SPR)s12650-022-00869-0-e DE-627 ger DE-627 rakwb eng Seo, Heerim verfasserin aut Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract Jet Impingement (dpeaa)DE-He213 Effusion Holes (dpeaa)DE-He213 Wall Jet (dpeaa)DE-He213 Concave Surface (dpeaa)DE-He213 PIV (dpeaa)DE-He213 CFD (dpeaa)DE-He213 Turbulence Model (dpeaa)DE-He213 Kwon, Daehee aut Lee, Seungju aut Yeom, Eunseop (orcid)0000-0002-9717-030X aut Enthalten in Journal of visualization Berlin : Springer, 1998 26(2022), 1 vom: 30. Aug., Seite 61-81 (DE-627)357174291 (DE-600)2094841-4 1875-8975 nnns volume:26 year:2022 number:1 day:30 month:08 pages:61-81 https://dx.doi.org/10.1007/s12650-022-00869-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 26 2022 1 30 08 61-81 |
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Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. 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Seo, Heerim |
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Seo, Heerim misc Jet Impingement misc Effusion Holes misc Wall Jet misc Concave Surface misc PIV misc CFD misc Turbulence Model Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system |
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Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system Jet Impingement (dpeaa)DE-He213 Effusion Holes (dpeaa)DE-He213 Wall Jet (dpeaa)DE-He213 Concave Surface (dpeaa)DE-He213 PIV (dpeaa)DE-He213 CFD (dpeaa)DE-He213 Turbulence Model (dpeaa)DE-He213 |
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Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system |
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Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system |
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Seo, Heerim Kwon, Daehee Lee, Seungju Yeom, Eunseop |
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experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system |
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Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system |
| abstract |
Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
| abstractGer |
Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
| abstract_unstemmed |
Impingement/effusion cooling is the most common cooling technique or the leading edge region of a gas turbine blade to increase the maximum allowable turbine inlet temperature and thermal efficiency. This study investigated the flow characteristics of jet impingement onto a concave target plate with effusion holes depending on the shape parameters using experimental and numerical analysis methods. The diameter of the injection plate and the arrangement of the effusion holes were varied at a jet Reynolds number of 5,000. The velocity fields were measured using the PIV technique in nine cases. The CFD results were validated through comparison with experimental results, and the 3D flow structures were estimated by computational fluid dynamics (CFD) simulations. The results are expected to provide knowledge for the design optimization of a cooling system to prevent the thermal load of the leading edge of gas turbine blades. Graphical abstract © The Visualization Society of Japan 2022. Springer Nature or its licensor holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
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Experimental and numerical investigation of the effects of the jet diameter and arrangement of effusion holes on the concave surface of an impingement/effusion cooling system |
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https://dx.doi.org/10.1007/s12650-022-00869-0 |
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Kwon, Daehee Lee, Seungju Yeom, Eunseop |
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Kwon, Daehee Lee, Seungju Yeom, Eunseop |
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10.1007/s12650-022-00869-0 |
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2024-07-03T23:49:09.539Z |
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| score |
7.402112 |