Schneider, Marius ; Schiffer, Heinz-Peter ; Lehmann, Knut (2023)
Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations.
In: International Journal of Turbomachinery, Propulsion and Power, 2017, 2 (4)
doi: 10.26083/tuprints-00015434
Artikel, Zweitveröffentlichung, Verlagsversion
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Kurzbeschreibung (Abstract)
An algorithm is presented generating a complete set of inlet boundary conditions for Reynolds-averaged Navier–Stokes computational fluid dynamics (RANS CFD) of high-pressure turbines to investigate their interaction with lean and rich burn combustors. The method shall contribute to understanding the sensitivities of turbine aerothermal performance in a systematic approach. The boundary conditions are based on a set of input parameters controlling velocity, temperature, and turbulence fields. All other quantities are derived from operating conditions and additional modelling assumptions. The algorithm is coupled with a CFD solver by applying the generated profiles as inlet boundary conditions. The successive steps to derive consistent flow profiles are described and results are validated against flow fields extracted from combustor CFD.
| Typ des Eintrags: | Artikel |
|---|---|
| Erschienen: | 2023 |
| Autor(en): | Schneider, Marius ; Schiffer, Heinz-Peter ; Lehmann, Knut |
| Art des Eintrags: | Zweitveröffentlichung |
| Titel: | Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations |
| Sprache: | Englisch |
| Publikationsjahr: | 27 November 2023 |
| Ort: | Darmstadt |
| Publikationsdatum der Erstveröffentlichung: | 2017 |
| Ort der Erstveröffentlichung: | Basel |
| Verlag: | MDPI |
| Titel der Zeitschrift, Zeitung oder Schriftenreihe: | International Journal of Turbomachinery, Propulsion and Power |
| Jahrgang/Volume einer Zeitschrift: | 2 |
| (Heft-)Nummer: | 4 |
| Kollation: | 21 Seiten |
| DOI: | 10.26083/tuprints-00015434 |
| URL / URN: | https://tuprints.ulb.tu-darmstadt.de/15434 |
| Zugehörige Links: | |
| Herkunft: | Zweitveröffentlichung DeepGreen |
| Kurzbeschreibung (Abstract): | An algorithm is presented generating a complete set of inlet boundary conditions for Reynolds-averaged Navier–Stokes computational fluid dynamics (RANS CFD) of high-pressure turbines to investigate their interaction with lean and rich burn combustors. The method shall contribute to understanding the sensitivities of turbine aerothermal performance in a systematic approach. The boundary conditions are based on a set of input parameters controlling velocity, temperature, and turbulence fields. All other quantities are derived from operating conditions and additional modelling assumptions. The algorithm is coupled with a CFD solver by applying the generated profiles as inlet boundary conditions. The successive steps to derive consistent flow profiles are described and results are validated against flow fields extracted from combustor CFD. |
| Freie Schlagworte: | computational fluid dynamics, combustor turbine interaction, axial turbine, boundary conditions |
| ID-Nummer: | 20 |
| Status: | Verlagsversion |
| URN: | urn:nbn:de:tuda-tuprints-154343 |
| Zusätzliche Informationen: | This article belongs to the Special Issue Selected Papers from the 12th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics (ETC12) |
| Sachgruppe der Dewey Dezimalklassifikatin (DDC): | 600 Technik, Medizin, angewandte Wissenschaften > 620 Ingenieurwissenschaften und Maschinenbau |
| Fachbereich(e)/-gebiet(e): | 16 Fachbereich Maschinenbau 16 Fachbereich Maschinenbau > Fachgebiet für Gasturbinen, Luft- und Raumfahrtantriebe (GLR) |
| Hinterlegungsdatum: | 27 Nov 2023 14:13 |
| Letzte Änderung: | 28 Nov 2023 06:34 |
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| Suche nach Titel in: | TUfind oder in Google |
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- Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations. (deposited 27 Nov 2023 14:13) [Gegenwärtig angezeigt]
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