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Cryogenic fluid jets and mixing layers in transcritical and supercritical environments

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TLDR
In this article, the authors provide an overview of recent advances in the theoretical modeling and numerical simulation of cryogenic fluid injection and mixing in transcritical and supercritical environments, using a general theoretical and numerical framework that accommodates full conservation laws and real-fluid thermodynamic and transport phenomena.
Abstract
This paper provides an overview of recent advances in the theoretical modeling and numerical simulation of cryogenic fluid injection and mixing in transcritical and supercritical environments. The basis of the analysis is a general theoretical and numerical framework that accommodates full conservation laws and real-fluid thermodynamic and transport phenomena. All of the thermophysical properties are determined directly from fundamental thermodynamics theories, along with the use of corresponding-state principles. Turbulence closure is achieved using a large-eddy-simulation technique, in which large-scale motions are calculated explicitly and the effects of unresolved small-scale turbulence are modeled either analytically or empirically. The analysis has been applied to study: (1) fluid jet dynamics, (2) swirl injection of liquid oxygen through a simplex swirl injector, and (3) shear co-axial injection and mixing of liquid oxygen and methane. Various effects, including density stratification, she...

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Journal ArticleDOI

On the transition between two-phase and single-phase interface dynamics in multicomponent fluids at supercritical pressures

TL;DR: In this paper, a model for the transition from two-phase spray atomization to single-phase diffusion-dominated mixing is presented, based on a modified 32-term Benedict-Webb-Rubin equation of state.
Journal ArticleDOI

Structure and dynamics of cryogenic flames at supercritical pressure

TL;DR: In this article, a detailed understanding of liquid propellant combustion is provided for the development of improved and more reliable propulsion systems, and experimental investigations aimed at providing such a fundamental basis for design and engineering of combustion components are described.
Journal ArticleDOI

Recent Experimental Efforts on High-Pressure Supercritical Injection for Liquid Rockets and Their Implications

TL;DR: In this paper, the authors present a summary of experimental achievements pertinent to liquid rockets, focusing only on the injection of nonreacting cryogenic liquids into a high-pressure environment surpassing the critical point of at least one of the injected fluids.
Journal ArticleDOI

Large-Eddy Simulation of Supercritical-Pressure Round Jets

TL;DR: In this article, a large-eddy simulation framework for turbulence modeling is used and real-gas effects are accounted for through a cubic equation of state and appropriate viscosity and conductivity coefficients.
Journal ArticleDOI

Understanding high-pressure gas-liquid interface phenomena in Diesel engines

TL;DR: In this article, a coupled model is proposed to obtain a theoretical analysis that quantifies under what conditions the interfacial dynamics transition between the classical non-continuum "jump" conditions associated with two phase flows and a continuous gas-liquid interfacial diffusion layer.
References
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Journal ArticleDOI

Perturbed Free Shear Layers

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The compressible turbulent shear layer: an experimental study

TL;DR: In this paper, the growth rate and turbulent structure of the compressible, plane shear layer are investigated experimentally in a novel facility, where it is possible to flow similar or dissimilar gases of different densities and to select different Mach numbers for each stream.
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Toward the large-eddy simulation of compressible turbulent flows

TL;DR: In this paper, a compressible generalization of the linear combination of the Smagorinsky model and scale-similarity model, in terms of Favre-filtered fields, is obtained for the subgrid-scale stress tensor.
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Two-dimensional shear-layer entrainment

TL;DR: In this article, a simple argument is proposed, based on the geometrical properties of the large-scale now structures of the subsonic, fully developed, two-dimensional mixing layer, which yields the entrainment ratio and growth of the turbulent mixing layer.
Journal ArticleDOI

On Central-Difference and Upwind Schemes

TL;DR: In this paper, a class of numerical dissipation models for central-difference schemes constructed with second and fourth difference terms is considered, where the notion of matrix dissipation associated with upwind schemes is used to establish improved shock capturing capability for these models.
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