2016
DOI: 10.2514/1.b35827
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Large-Eddy Simulation of Coaxial LN2/GH2 Injection at Trans- and Supercritical Conditions

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Cited by 47 publications
(16 citation statements)
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“…In order to investigate high-pressure injection, large-eddy simulations have been carried out with two different solvers. These solvers have been extensively used for supercritical injection simulations of both pure as well as binary jets, see e.g., [8,11,16], whereby one of those solvers is the density-based INCA (www.inca-cfd.com) and the other is a pressure-based version of OpenFOAM (www.openfoam.org). For the reason of clarity and with thermodynamic aspects being the main objective -not the cross-comparison of LES codes -only one set of LES results (INCA) is presented in this paper.…”
Section: Methodsmentioning
confidence: 99%
“…In order to investigate high-pressure injection, large-eddy simulations have been carried out with two different solvers. These solvers have been extensively used for supercritical injection simulations of both pure as well as binary jets, see e.g., [8,11,16], whereby one of those solvers is the density-based INCA (www.inca-cfd.com) and the other is a pressure-based version of OpenFOAM (www.openfoam.org). For the reason of clarity and with thermodynamic aspects being the main objective -not the cross-comparison of LES codes -only one set of LES results (INCA) is presented in this paper.…”
Section: Methodsmentioning
confidence: 99%
“…Hickey et al [6] used a second-order accurate Essentially Non-Oscillating (ENO) scheme which was switched to a first-order upwind scheme in gradient regions. Similar approach have been used by Park et al [41], Muller et al [42] and Matheis et al [43]. Dissipation was also introduced via artificial diffusion schemes.…”
Section: Introductionmentioning
confidence: 92%
“…The code uses a pressurebased solution approach for transonic flows based on the compressible version of the PISO method and employs second order linear differences for spatial discretization. Recently, the framework has been used to study both non-reacting 13,14 and reacting 15 flows at rocket-like conditions. In the present contribution, the combustor was simulated with large eddy simulation resolving the larger turbulent scales, while closing the subgrid-scale turbulence using the Vreman model.…”
Section: Institute For Thermodynamics (Unibw) Universität Der Bunmentioning
confidence: 99%