Influence of trailing-edge grid structure on Navier-Stokes computation of turbomachinery cascade flow
Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the per...
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1992 |
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| Umfang: |
6 Ill. 12 |
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| Reproduktion: |
Wiley InterScience Backfile Collection 1832-2000 |
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| Übergeordnetes Werk: |
in: International Journal for Numerical Methods in Fluids - Chichester : Wiley, 15(1992) vom: Aug., Seite 883-894 |
| Übergeordnetes Werk: |
volume:15 ; year:1992 ; month:08 ; pages:883-894 ; extent:12 |
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NLEJ163220727 |
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| 520 | |a Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. | ||
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(DE-627)NLEJ163220727 DE-627 ger DE-627 rakwb eng Influence of trailing-edge grid structure on Navier-Stokes computation of turbomachinery cascade flow 1992 6 Ill. 12 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. Wiley InterScience Backfile Collection 1832-2000 Chung, Hee-Taeg oth Baek, Je-Hyun oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 15(1992) vom: Aug., Seite 883-894 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:15 year:1992 month:08 pages:883-894 extent:12 http://dx.doi.org/10.1002/fld.1650150804 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 15 1992 8 883-894 12 |
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(DE-627)NLEJ163220727 DE-627 ger DE-627 rakwb eng Influence of trailing-edge grid structure on Navier-Stokes computation of turbomachinery cascade flow 1992 6 Ill. 12 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. Wiley InterScience Backfile Collection 1832-2000 Chung, Hee-Taeg oth Baek, Je-Hyun oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 15(1992) vom: Aug., Seite 883-894 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:15 year:1992 month:08 pages:883-894 extent:12 http://dx.doi.org/10.1002/fld.1650150804 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 15 1992 8 883-894 12 |
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(DE-627)NLEJ163220727 DE-627 ger DE-627 rakwb eng Influence of trailing-edge grid structure on Navier-Stokes computation of turbomachinery cascade flow 1992 6 Ill. 12 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. Wiley InterScience Backfile Collection 1832-2000 Chung, Hee-Taeg oth Baek, Je-Hyun oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 15(1992) vom: Aug., Seite 883-894 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:15 year:1992 month:08 pages:883-894 extent:12 http://dx.doi.org/10.1002/fld.1650150804 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 15 1992 8 883-894 12 |
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(DE-627)NLEJ163220727 DE-627 ger DE-627 rakwb eng Influence of trailing-edge grid structure on Navier-Stokes computation of turbomachinery cascade flow 1992 6 Ill. 12 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. Wiley InterScience Backfile Collection 1832-2000 Chung, Hee-Taeg oth Baek, Je-Hyun oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 15(1992) vom: Aug., Seite 883-894 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:15 year:1992 month:08 pages:883-894 extent:12 http://dx.doi.org/10.1002/fld.1650150804 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 15 1992 8 883-894 12 |
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(DE-627)NLEJ163220727 DE-627 ger DE-627 rakwb eng Influence of trailing-edge grid structure on Navier-Stokes computation of turbomachinery cascade flow 1992 6 Ill. 12 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. Wiley InterScience Backfile Collection 1832-2000 Chung, Hee-Taeg oth Baek, Je-Hyun oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 15(1992) vom: Aug., Seite 883-894 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:15 year:1992 month:08 pages:883-894 extent:12 http://dx.doi.org/10.1002/fld.1650150804 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 15 1992 8 883-894 12 |
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influence of trailing-edge grid structure on navier-stokes computation of turbomachinery cascade flow |
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Influence of trailing-edge grid structure on Navier-Stokes computation of turbomachinery cascade flow |
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Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. |
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Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. |
| abstract_unstemmed |
Three kinds of grid system based on C-type grid are examined in order to reveal their relative flow characteristics of the turbomachinery cascade, especially near the trailing edge and wake. Here, a semi-conservative interpolation technique to treat the discontinuous boundary condition along the periodic boundary is proposed and is applied on the patched-type grid structure. Computational results are presented to see the influence of trailing-edge grid structure on the Navier-Stokes solutions for the high-turning transonic turbine cascade. |
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