Numerical investigation of transverse hydrogen jet into supersonic crossflow using detached-eddy simulation

Su Hee Won; In Seuck Jeung; Bernard Parent; Jeong Yeol Choi

doi:10.2514/1.41165

Numerical investigation of transverse hydrogen jet into supersonic crossflow using detached-eddy simulation

Su Hee Won, In Seuck Jeung, Bernard Parent, Jeong Yeol Choi

Research output: Contribution to journal › Article › peer-review

69 Scopus citations

Abstract

A three-dimensional unsteady reacting flowfield that is generated by transverse hydrogen injection into a supersonic mainstream is numerically investigated using detached-eddy simulation and a finite-rate chemistry model. Grid refinement with the grid-convergence-index concept is applied to the instantaneous flowfield for assessing the grid resolution and solution convergence. Validation is performed for the jet penetration height, and the predicted result is in good agreement with experimental trends. The results indicate that jet vortical structures are generated as the interacting counter-rotating vortices become alternately detached in the upstream recirculation region. Although the numerical OH distribution reproduces the experimental OH-planar-laser-induced fluorescence well, there are some disparities in the ignition delay times due to the restricted availability of experimental and numerical data. The effects of the turbulence model on combustion are identified by a comparative analysis of the Reynolds-averaged Navier-Stokes and detached-eddy simulation approaches. Their effects are quantified by the production of H₂O, which is the primary species of hydrogen combustion.

Original language	English (US)
Pages (from-to)	1047-1058
Number of pages	12
Journal	AIAA journal
Volume	48
Issue number	6
DOIs	https://doi.org/10.2514/1.41165
State	Published - Jun 2010
Externally published	Yes

ASJC Scopus subject areas

Aerospace Engineering

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10.2514/1.41165

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title = "Numerical investigation of transverse hydrogen jet into supersonic crossflow using detached-eddy simulation",

abstract = "A three-dimensional unsteady reacting flowfield that is generated by transverse hydrogen injection into a supersonic mainstream is numerically investigated using detached-eddy simulation and a finite-rate chemistry model. Grid refinement with the grid-convergence-index concept is applied to the instantaneous flowfield for assessing the grid resolution and solution convergence. Validation is performed for the jet penetration height, and the predicted result is in good agreement with experimental trends. The results indicate that jet vortical structures are generated as the interacting counter-rotating vortices become alternately detached in the upstream recirculation region. Although the numerical OH distribution reproduces the experimental OH-planar-laser-induced fluorescence well, there are some disparities in the ignition delay times due to the restricted availability of experimental and numerical data. The effects of the turbulence model on combustion are identified by a comparative analysis of the Reynolds-averaged Navier-Stokes and detached-eddy simulation approaches. Their effects are quantified by the production of H2O, which is the primary species of hydrogen combustion.",

author = "Won, {Su Hee} and Jeung, {In Seuck} and Bernard Parent and Choi, {Jeong Yeol}",

note = "Funding Information: The present study was supported by the basic research grants of the Defense Acquisition Program Administration, through the Agency for Defense Development, and the National Research Foundation of Korea grant, funded by the Korean Government (Ministry of Education, Science, and Technology). The authors would like to thank Ronald K. Hanson of Stanford University and Adela Ben-Yakar of the University of Texas at Austin for providing experimental data and for informed discussions regarding this topic.",

year = "2010",

month = jun,

doi = "10.2514/1.41165",

language = "English (US)",

volume = "48",

pages = "1047--1058",

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issn = "0001-1452",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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AU - Won, Su Hee

AU - Jeung, In Seuck

AU - Parent, Bernard

AU - Choi, Jeong Yeol

N1 - Funding Information: The present study was supported by the basic research grants of the Defense Acquisition Program Administration, through the Agency for Defense Development, and the National Research Foundation of Korea grant, funded by the Korean Government (Ministry of Education, Science, and Technology). The authors would like to thank Ronald K. Hanson of Stanford University and Adela Ben-Yakar of the University of Texas at Austin for providing experimental data and for informed discussions regarding this topic.

PY - 2010/6

Y1 - 2010/6

N2 - A three-dimensional unsteady reacting flowfield that is generated by transverse hydrogen injection into a supersonic mainstream is numerically investigated using detached-eddy simulation and a finite-rate chemistry model. Grid refinement with the grid-convergence-index concept is applied to the instantaneous flowfield for assessing the grid resolution and solution convergence. Validation is performed for the jet penetration height, and the predicted result is in good agreement with experimental trends. The results indicate that jet vortical structures are generated as the interacting counter-rotating vortices become alternately detached in the upstream recirculation region. Although the numerical OH distribution reproduces the experimental OH-planar-laser-induced fluorescence well, there are some disparities in the ignition delay times due to the restricted availability of experimental and numerical data. The effects of the turbulence model on combustion are identified by a comparative analysis of the Reynolds-averaged Navier-Stokes and detached-eddy simulation approaches. Their effects are quantified by the production of H2O, which is the primary species of hydrogen combustion.

AB - A three-dimensional unsteady reacting flowfield that is generated by transverse hydrogen injection into a supersonic mainstream is numerically investigated using detached-eddy simulation and a finite-rate chemistry model. Grid refinement with the grid-convergence-index concept is applied to the instantaneous flowfield for assessing the grid resolution and solution convergence. Validation is performed for the jet penetration height, and the predicted result is in good agreement with experimental trends. The results indicate that jet vortical structures are generated as the interacting counter-rotating vortices become alternately detached in the upstream recirculation region. Although the numerical OH distribution reproduces the experimental OH-planar-laser-induced fluorescence well, there are some disparities in the ignition delay times due to the restricted availability of experimental and numerical data. The effects of the turbulence model on combustion are identified by a comparative analysis of the Reynolds-averaged Navier-Stokes and detached-eddy simulation approaches. Their effects are quantified by the production of H2O, which is the primary species of hydrogen combustion.

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Numerical investigation of transverse hydrogen jet into supersonic crossflow using detached-eddy simulation

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