Numerical Simulation of the Non-Reactive and Reactive Flow in a Swirled Model Gas Turbine Combustor-Reference-Cited by-同舟云学术

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Numerical Simulation of the Non-Reactive and Reactive Flow in a Swirled Model Gas Turbine Combustor

Published:2013-06-22 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

Reichling Gilles¹,Noll Berthold¹,Aigner Manfred¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2434

Reference139 articles.

1. model of Menter et al.22-26is used as a hybrid URANS/LES approach. Furthermore, measurements con

2. The first step can be seen as the predictor step of the CPM algorithm. The steps 2-7 represent the corrector

3. The k-ω-SST (Shear Stress Transport) turbulence model has been proposed by Menter21in 1994. In the

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1. Influence of the turbulence model on the numerical predictions of cold turbulent flow in a heavy-duty gas turbine DLN combustor;International Journal of Thermal Sciences;2024-02

2. Investigation of Flow and Fuel/Air Mixing in a Heavy-Duty Gas Turbine DLN Combustor Using Laser Diagnostics and Numerical Simulation;Springer Proceedings in Physics;2024

3. Experimental and Numerical Investigation of the Non-Reacting Flow in a High-Fidelity Heavy-Duty Gas Turbine DLN Combustor;Energies;2022-12-16

4. Experimental analysis of thermo-acoustic instabilities in a generic gas turbine combustor by phase-correlated PIV, chemiluminescence, and laser Raman scattering measurements;Experiments in Fluids;2015-03-18

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