Measurement and Simulation of Turbulent Mixing in a Jet in Crossflow

Author:

Galeazzo Flavio Cesar Cunha1,Donnert Georg1,Habisreuther Peter1,Zarzalis Nikolaos1,Valdes Richard J.2,Krebs Werner3

Affiliation:

1. Division of Combustion Technology, Engler-Bunte-Institute, Karlsruhe Institute of Technology, Engler-Bunte-Ring 1, 76131 Karlsruhe, Germany

2. Siemens Energy, Inc., EN 323, 4400 Alafaya Trail, MC Q3-042, Orlando, FL 32826

3. Siemens AG, PG PE3, Mellinghofer Str. 55, 45466 Muelheim an der Ruhr, Germany

Abstract

Computational fluid dynamics (CFD) has an important role in current research. While large eddy simulations (LES) are now common practice in academia, Reynolds-averaged Navier–Stokes (RANS) simulations are still very common in the industry. Using RANS allows faster simulations, however, the choice of the turbulence model has a bigger impact on the results. An important influence of the turbulence modeling is the description of turbulent mixing. Experience has shown that often inaccurate simulations of combustion processes originate from an inadequate description of the mixing field. A simple turbulent flow and mixing configuration of major theoretical and practical importance is the jet in crossflow (JIC). Due to its good fuel-air mixing capability over a small distance, JIC is favored by gas turbine manufacturers. As the design of the mixing process is the key to creating stable low NOx combustion systems, reliable predictive tools and detailed understanding of this basic system are still demanded. Therefore, the current study has re-investigated the JIC configuration under engine relevant conditions both experimentally and numerically using the most sophisticated tools available today. The combination of planar particle image velocimetry and laser induced fluorescence was used to measure the turbulent velocity and concentration fields as well as to determine the correlations of the Reynolds stress tensor ui′uj′¯ and the Reynolds flux vector ui′c′¯. Boundary conditions were determined using laser Doppler velocimetry. The comparisons between the measurements and simulation using RANS and LES showed that the mean velocity field was well described using the SST turbulence model. However, the Reynolds stresses and more so, the Reynolds fluxes deviate substantially from the measured data. The systematic variation of the turbulent Schmidt number reveals the limited influence of this parameter indicating that the basic modeling is amiss. The results of the LES simulation using the standard Smagorinsky model were found to provide much better agreement with the experiments also in the description of turbulent mixing.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference19 articles.

1. Mixing of Multiple Jets With a Confined Subsonic Crossflow: Part I—Cylindrical Duct;Holdeman;ASME J. Eng. Gas Turbines Power

2. Predictions of Momentum and Scalar Fields in a Jet in Cross-Flow Using First and Second Order Turbulence Closures;Alvarez

3. Fifty Years of Jet in Cross Flow Research;Margason

4. Simultaneous Measurements of Scalar and Velocity Field Evolution in Turbulent Crossflowing Jets;Su;J. Fluid Mech.

5. Two-Dimensional Estimation of Reynolds-Fluxes and -Stresses in a Jet-in-Crossflow Arrangement by Simultaneous 2D-LIF and PIV;Cárdenas;Appl. Phys. B: Lasers Opt.

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