Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets
High-pressure jet injection into quiescent air is a challenging fluid dynamics problem in the field of aerospace engineering. Although plenty of experimental, theoretical, and numerical studies have been conducted to explore this flow, there is a dearth of literature detailing the flow evolution and...
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description | High-pressure jet injection into quiescent air is a challenging fluid dynamics problem in the field of aerospace engineering. Although plenty of experimental, theoretical, and numerical studies have been conducted to explore this flow, there is a dearth of literature detailing the flow evolution and instability characteristics, which is vital to the mixing enhancement design and jet noise reduction. In this paper, a density-based solver for compressible supersonic flow, astroFoam, is developed based on the OpenFOAM library. Large-eddy simulations of highly underexpanded jets with nozzle pressure ratios from 5.60 to 11.21 at a Reynolds number around 105 are carried out with a high-resolution grid. A grid-convergence study has been conducted to confirm the fidelity of the large-eddy simulation results. The large-eddy simulation results have also been validated against available literature data in terms of the time-averaged near-field properties of underexpanded jets. The turbulent transition processes are revealed based on the instantaneous flow features and are quantitatively resolved according to the jet penetration and maximum width. The vorticity analysis is conducted to understand the turbulent transition mechanism, and it is found that the vortex stretching term plays a leading role on the distortion of the vortex rings in the near field of the jets. The dominant instability modes of jets, visualized by helicity, are quantitatively revealed based on the spectrum and relative phase of pressure fluctuation. The single helical modes corresponding to a phase angle close to ±180 deg with the 1+1 helices are dominant for nozzle pressure ratios of 5.60 and 7.47, whereas the complex and multiple helices for the other two higher nozzle pressure ratios are due to the superposition of the single and double helical modes. In addition, the performance of the coarse mesh and different subgrid-scale models on capturing the dominant instability characteristics in large-eddy simulation of underexpanded jets is investigated. |
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Although plenty of experimental, theoretical, and numerical studies have been conducted to explore this flow, there is a dearth of literature detailing the flow evolution and instability characteristics, which is vital to the mixing enhancement design and jet noise reduction. In this paper, a density-based solver for compressible supersonic flow, astroFoam, is developed based on the OpenFOAM library. Large-eddy simulations of highly underexpanded jets with nozzle pressure ratios from 5.60 to 11.21 at a Reynolds number around 105 are carried out with a high-resolution grid. A grid-convergence study has been conducted to confirm the fidelity of the large-eddy simulation results. The large-eddy simulation results have also been validated against available literature data in terms of the time-averaged near-field properties of underexpanded jets. The turbulent transition processes are revealed based on the instantaneous flow features and are quantitatively resolved according to the jet penetration and maximum width. The vorticity analysis is conducted to understand the turbulent transition mechanism, and it is found that the vortex stretching term plays a leading role on the distortion of the vortex rings in the near field of the jets. The dominant instability modes of jets, visualized by helicity, are quantitatively revealed based on the spectrum and relative phase of pressure fluctuation. The single helical modes corresponding to a phase angle close to ±180 deg with the 1+1 helices are dominant for nozzle pressure ratios of 5.60 and 7.47, whereas the complex and multiple helices for the other two higher nozzle pressure ratios are due to the superposition of the single and double helical modes. In addition, the performance of the coarse mesh and different subgrid-scale models on capturing the dominant instability characteristics in large-eddy simulation of underexpanded jets is investigated.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J054689</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Aerospace engineering ; Compressibility ; Computational fluid dynamics ; Evolution ; Finite element method ; Flow stability ; Fluid flow ; Helices ; Helicity ; Jet aircraft noise ; Large eddy simulation ; Near fields ; Noise reduction ; Nozzles ; Reynolds number ; Scale models ; Simulation ; Supersonic flow ; Vortex rings ; Vortices ; Vorticity</subject><ispartof>AIAA journal, 2016-10, Vol.54 (10), p.3191-3211</ispartof><rights>Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal and internal use, on condition that the copier pay the per-copy fee to the Copyright Clearance Center (CCC). All requests for copying and permission to reprint should be submitted to CCC at ; employ the ISSN (print) or (online) to initiate your request.</rights><rights>Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal and internal use, on condition that the copier pay the per-copy fee to the Copyright Clearance Center (CCC). All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a389t-388bd8602aa5e215b98c4cdf2bb9c076bdeda07b6ef9b55c650b48a54af73b43</citedby><cites>FETCH-LOGICAL-a389t-388bd8602aa5e215b98c4cdf2bb9c076bdeda07b6ef9b55c650b48a54af73b43</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>315,782,786,27933,27934</link.rule.ids></links><search><creatorcontrib>Li, Xiaopeng</creatorcontrib><creatorcontrib>Yao, Wei</creatorcontrib><creatorcontrib>Fan, Xuejun</creatorcontrib><title>Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets</title><title>AIAA journal</title><description>High-pressure jet injection into quiescent air is a challenging fluid dynamics problem in the field of aerospace engineering. Although plenty of experimental, theoretical, and numerical studies have been conducted to explore this flow, there is a dearth of literature detailing the flow evolution and instability characteristics, which is vital to the mixing enhancement design and jet noise reduction. In this paper, a density-based solver for compressible supersonic flow, astroFoam, is developed based on the OpenFOAM library. Large-eddy simulations of highly underexpanded jets with nozzle pressure ratios from 5.60 to 11.21 at a Reynolds number around 105 are carried out with a high-resolution grid. A grid-convergence study has been conducted to confirm the fidelity of the large-eddy simulation results. The large-eddy simulation results have also been validated against available literature data in terms of the time-averaged near-field properties of underexpanded jets. The turbulent transition processes are revealed based on the instantaneous flow features and are quantitatively resolved according to the jet penetration and maximum width. The vorticity analysis is conducted to understand the turbulent transition mechanism, and it is found that the vortex stretching term plays a leading role on the distortion of the vortex rings in the near field of the jets. The dominant instability modes of jets, visualized by helicity, are quantitatively revealed based on the spectrum and relative phase of pressure fluctuation. The single helical modes corresponding to a phase angle close to ±180 deg with the 1+1 helices are dominant for nozzle pressure ratios of 5.60 and 7.47, whereas the complex and multiple helices for the other two higher nozzle pressure ratios are due to the superposition of the single and double helical modes. In addition, the performance of the coarse mesh and different subgrid-scale models on capturing the dominant instability characteristics in large-eddy simulation of underexpanded jets is investigated.</description><subject>Aerodynamics</subject><subject>Aerospace engineering</subject><subject>Compressibility</subject><subject>Computational fluid dynamics</subject><subject>Evolution</subject><subject>Finite element method</subject><subject>Flow stability</subject><subject>Fluid flow</subject><subject>Helices</subject><subject>Helicity</subject><subject>Jet aircraft noise</subject><subject>Large eddy simulation</subject><subject>Near fields</subject><subject>Noise reduction</subject><subject>Nozzles</subject><subject>Reynolds number</subject><subject>Scale models</subject><subject>Simulation</subject><subject>Supersonic flow</subject><subject>Vortex rings</subject><subject>Vortices</subject><subject>Vorticity</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNpl0FFLwzAQB_AgCs7pg98gIAg-dCZN0qaPMja3MfBhE8SXcGnSmdG1M2nFfns7N_DBp-OOH_87DqFbSkaxoPyRjhZE8ERmZ2hABWMRk-LtHA0IITSiXMSX6CqEbd_FqaQD9L4Ev7HRxJgOr9yuLaFxdYXrAq_dzuLJV122vxOoDJ5XoQHtStd0BzFzm4-yw6-Vsd5-73thDV7VlcvxwjbhGl0UUAZ7c6pDtJ5O1uNZtHx5no-flhEwmTX9gVIbmZAYQNiYCp3JnOemiLXOcpImuk8FkurEFpkWIk8E0VyC4FCkTHM2RHfH2L2vP1sbGrWtW1_1G1XMM8oYk_ygHo4q93UI3hZq790OfKcoUYfPKapOn-vt_dGCA_hL-w9_AFvWbGE</recordid><startdate>20161001</startdate><enddate>20161001</enddate><creator>Li, Xiaopeng</creator><creator>Yao, Wei</creator><creator>Fan, Xuejun</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20161001</creationdate><title>Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets</title><author>Li, Xiaopeng ; Yao, Wei ; Fan, Xuejun</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a389t-388bd8602aa5e215b98c4cdf2bb9c076bdeda07b6ef9b55c650b48a54af73b43</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Aerodynamics</topic><topic>Aerospace engineering</topic><topic>Compressibility</topic><topic>Computational fluid dynamics</topic><topic>Evolution</topic><topic>Finite element method</topic><topic>Flow stability</topic><topic>Fluid flow</topic><topic>Helices</topic><topic>Helicity</topic><topic>Jet aircraft noise</topic><topic>Large eddy simulation</topic><topic>Near fields</topic><topic>Noise reduction</topic><topic>Nozzles</topic><topic>Reynolds number</topic><topic>Scale models</topic><topic>Simulation</topic><topic>Supersonic flow</topic><topic>Vortex rings</topic><topic>Vortices</topic><topic>Vorticity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Li, Xiaopeng</creatorcontrib><creatorcontrib>Yao, Wei</creatorcontrib><creatorcontrib>Fan, Xuejun</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Li, Xiaopeng</au><au>Yao, Wei</au><au>Fan, Xuejun</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets</atitle><jtitle>AIAA journal</jtitle><date>2016-10-01</date><risdate>2016</risdate><volume>54</volume><issue>10</issue><spage>3191</spage><epage>3211</epage><pages>3191-3211</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>High-pressure jet injection into quiescent air is a challenging fluid dynamics problem in the field of aerospace engineering. Although plenty of experimental, theoretical, and numerical studies have been conducted to explore this flow, there is a dearth of literature detailing the flow evolution and instability characteristics, which is vital to the mixing enhancement design and jet noise reduction. In this paper, a density-based solver for compressible supersonic flow, astroFoam, is developed based on the OpenFOAM library. Large-eddy simulations of highly underexpanded jets with nozzle pressure ratios from 5.60 to 11.21 at a Reynolds number around 105 are carried out with a high-resolution grid. A grid-convergence study has been conducted to confirm the fidelity of the large-eddy simulation results. The large-eddy simulation results have also been validated against available literature data in terms of the time-averaged near-field properties of underexpanded jets. The turbulent transition processes are revealed based on the instantaneous flow features and are quantitatively resolved according to the jet penetration and maximum width. The vorticity analysis is conducted to understand the turbulent transition mechanism, and it is found that the vortex stretching term plays a leading role on the distortion of the vortex rings in the near field of the jets. The dominant instability modes of jets, visualized by helicity, are quantitatively revealed based on the spectrum and relative phase of pressure fluctuation. The single helical modes corresponding to a phase angle close to ±180 deg with the 1+1 helices are dominant for nozzle pressure ratios of 5.60 and 7.47, whereas the complex and multiple helices for the other two higher nozzle pressure ratios are due to the superposition of the single and double helical modes. In addition, the performance of the coarse mesh and different subgrid-scale models on capturing the dominant instability characteristics in large-eddy simulation of underexpanded jets is investigated.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J054689</doi><tpages>21</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aerodynamics Aerospace engineering Compressibility Computational fluid dynamics Evolution Finite element method Flow stability Fluid flow Helices Helicity Jet aircraft noise Large eddy simulation Near fields Noise reduction Nozzles Reynolds number Scale models Simulation Supersonic flow Vortex rings Vortices Vorticity |
title | Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets |
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