Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach
The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant nu...
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1986 |
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| Umfang: |
5 Ill. 7 |
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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, 6(1986) vom: Juni, Seite 387-393 |
| Übergeordnetes Werk: |
volume:6 ; year:1986 ; month:06 ; pages:387-393 ; extent:7 |
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| 245 | 1 | 0 | |a Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach |
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| 520 | |a The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. | ||
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| 700 | 1 | |a Swaminathan, V. |4 oth | |
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(DE-627)NLEJ163211981 DE-627 ger DE-627 rakwb eng Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach 1986 5 Ill. 7 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. Wiley InterScience Backfile Collection 1832-2000 Madhavan, N. S. oth Swaminathan, V. oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 6(1986) vom: Juni, Seite 387-393 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:6 year:1986 month:06 pages:387-393 extent:7 http://dx.doi.org/10.1002/fld.1650060606 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 6 1986 6 387-393 7 |
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(DE-627)NLEJ163211981 DE-627 ger DE-627 rakwb eng Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach 1986 5 Ill. 7 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. Wiley InterScience Backfile Collection 1832-2000 Madhavan, N. S. oth Swaminathan, V. oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 6(1986) vom: Juni, Seite 387-393 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:6 year:1986 month:06 pages:387-393 extent:7 http://dx.doi.org/10.1002/fld.1650060606 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 6 1986 6 387-393 7 |
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(DE-627)NLEJ163211981 DE-627 ger DE-627 rakwb eng Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach 1986 5 Ill. 7 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. Wiley InterScience Backfile Collection 1832-2000 Madhavan, N. S. oth Swaminathan, V. oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 6(1986) vom: Juni, Seite 387-393 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:6 year:1986 month:06 pages:387-393 extent:7 http://dx.doi.org/10.1002/fld.1650060606 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 6 1986 6 387-393 7 |
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(DE-627)NLEJ163211981 DE-627 ger DE-627 rakwb eng Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach 1986 5 Ill. 7 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. Wiley InterScience Backfile Collection 1832-2000 Madhavan, N. S. oth Swaminathan, V. oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 6(1986) vom: Juni, Seite 387-393 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:6 year:1986 month:06 pages:387-393 extent:7 http://dx.doi.org/10.1002/fld.1650060606 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 6 1986 6 387-393 7 |
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(DE-627)NLEJ163211981 DE-627 ger DE-627 rakwb eng Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach 1986 5 Ill. 7 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. Wiley InterScience Backfile Collection 1832-2000 Madhavan, N. S. oth Swaminathan, V. oth in International Journal for Numerical Methods in Fluids Chichester : Wiley 6(1986) vom: Juni, Seite 387-393 (DE-627)NLEJ159071224 (DE-600)1491176-0 0271-2091 nnns volume:6 year:1986 month:06 pages:387-393 extent:7 http://dx.doi.org/10.1002/fld.1650060606 text/html Deutschlandweit zugänglich GBV_USEFLAG_U ZDB-1-WIS GBV_NL_ARTICLE AR 6 1986 6 387-393 7 |
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numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach |
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Numerical solution of the supersonic laminar flow over a two-dimensional compression corner using an implicit approach |
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The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. |
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The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. |
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The use of an implicit numerical scheme, analogous to MacCormack's1, for the supersonic laminar two-dimensional compression corner flow problem using unsteady Navier-Stokes equations is demonstrated. The technique entails a reduction of about 70 per cent in the computation time for a Courant number of 5, but it is characterized by an increase of approximately 20 per cent in computer memory requirement. |
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