Experimental and numerical study of space station airflow distribution under microgravity condition
A space station that operates under microgravity conditions is a closed environment where a reasonable airflow distribution is required to eliminate body heat dissipation, remove contaminants and thus keep the crew comfortable. However, design of a reasonable airflow distribution has remained challe...
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Veröffentlicht in: | Building and environment 2018-10, Vol.144, p.268-280 |
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creator | Wang, Congcong Liu, Junjie Shang, Wenjin Sun, Hejiang Li, Jiayu Fan, Fenghua |
description | A space station that operates under microgravity conditions is a closed environment where a reasonable airflow distribution is required to eliminate body heat dissipation, remove contaminants and thus keep the crew comfortable. However, design of a reasonable airflow distribution has remained challenging. In this study, a computational fluid dynamics (CFD) methods with various turbulence models were used to investigate the airflow distribution inside a space station under microgravity conditions. To compare the performance of different models, the shrinkable ratio method was used to set up a mockup station to eliminate the influence of gravity-induced natural convection. The air velocity distribution in the narrow scale model was measured using particle image velocimetry (PIV). Results showed that the performance of the standard k-ε turbulence model was better than the renormalized group (RNG) k-ε turbulence model. The air distribution was optimized by changing the angle of the air supply outlet, suggesting that a three-dimensional air supply can provide better thermal comfort and higher air quality.
•CFD method was used to study the airflow distribution in enclosure under microgravity conditions.•Shrinkable ratio method was used to eliminate the influence of natural convection on airflow at ground test.•Airflow in the shrinkable ratio model was measured using PIV technique.•Three-dimensional air supply can provide more reasonable velocity distribution than vertical air supply. |
doi_str_mv | 10.1016/j.buildenv.2018.08.017 |
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•CFD method was used to study the airflow distribution in enclosure under microgravity conditions.•Shrinkable ratio method was used to eliminate the influence of natural convection on airflow at ground test.•Airflow in the shrinkable ratio model was measured using PIV technique.•Three-dimensional air supply can provide more reasonable velocity distribution than vertical air supply.</description><identifier>ISSN: 0360-1323</identifier><identifier>EISSN: 1873-684X</identifier><identifier>DOI: 10.1016/j.buildenv.2018.08.017</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Aerodynamics ; Air flow ; Air quality ; CFD ; Computational fluid dynamics ; Computer applications ; Contaminants ; Convection ; Fluid dynamics ; Fluid flow ; Free convection ; Hydrodynamics ; K-epsilon turbulence model ; Microgravity ; Numerical analysis ; Particle image velocimetry ; Pollutant removal ; Scale models ; Shrinkable ratio method ; Space stations ; Thermal comfort ; Thermal energy ; Turbulence ; Turbulence models ; Velocity distribution ; Velocity measurement ; Weightlessness</subject><ispartof>Building and environment, 2018-10, Vol.144, p.268-280</ispartof><rights>2018 Elsevier Ltd</rights><rights>Copyright Elsevier BV Oct 15, 2018</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c340t-6140a18f4ee5bb7d6acd3f30f46ff1d518d8b70fa4c31e8c62032a98d460090a3</citedby><cites>FETCH-LOGICAL-c340t-6140a18f4ee5bb7d6acd3f30f46ff1d518d8b70fa4c31e8c62032a98d460090a3</cites><orcidid>0000-0001-6895-5522 ; 0000-0002-5398-1151</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.buildenv.2018.08.017$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3548,27922,27923,45993</link.rule.ids></links><search><creatorcontrib>Wang, Congcong</creatorcontrib><creatorcontrib>Liu, Junjie</creatorcontrib><creatorcontrib>Shang, Wenjin</creatorcontrib><creatorcontrib>Sun, Hejiang</creatorcontrib><creatorcontrib>Li, Jiayu</creatorcontrib><creatorcontrib>Fan, Fenghua</creatorcontrib><title>Experimental and numerical study of space station airflow distribution under microgravity condition</title><title>Building and environment</title><description>A space station that operates under microgravity conditions is a closed environment where a reasonable airflow distribution is required to eliminate body heat dissipation, remove contaminants and thus keep the crew comfortable. However, design of a reasonable airflow distribution has remained challenging. In this study, a computational fluid dynamics (CFD) methods with various turbulence models were used to investigate the airflow distribution inside a space station under microgravity conditions. To compare the performance of different models, the shrinkable ratio method was used to set up a mockup station to eliminate the influence of gravity-induced natural convection. The air velocity distribution in the narrow scale model was measured using particle image velocimetry (PIV). Results showed that the performance of the standard k-ε turbulence model was better than the renormalized group (RNG) k-ε turbulence model. The air distribution was optimized by changing the angle of the air supply outlet, suggesting that a three-dimensional air supply can provide better thermal comfort and higher air quality.
•CFD method was used to study the airflow distribution in enclosure under microgravity conditions.•Shrinkable ratio method was used to eliminate the influence of natural convection on airflow at ground test.•Airflow in the shrinkable ratio model was measured using PIV technique.•Three-dimensional air supply can provide more reasonable velocity distribution than vertical air supply.</description><subject>Aerodynamics</subject><subject>Air flow</subject><subject>Air quality</subject><subject>CFD</subject><subject>Computational fluid dynamics</subject><subject>Computer applications</subject><subject>Contaminants</subject><subject>Convection</subject><subject>Fluid dynamics</subject><subject>Fluid flow</subject><subject>Free convection</subject><subject>Hydrodynamics</subject><subject>K-epsilon turbulence model</subject><subject>Microgravity</subject><subject>Numerical analysis</subject><subject>Particle image velocimetry</subject><subject>Pollutant removal</subject><subject>Scale models</subject><subject>Shrinkable ratio method</subject><subject>Space stations</subject><subject>Thermal comfort</subject><subject>Thermal energy</subject><subject>Turbulence</subject><subject>Turbulence models</subject><subject>Velocity distribution</subject><subject>Velocity measurement</subject><subject>Weightlessness</subject><issn>0360-1323</issn><issn>1873-684X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNqFUNtKxDAQDaLguvoLEvC5ddJk0_ZNWdYLCL4o-BbSXCSlm6xJu7p_b9bVZ-HAMJczM-cgdEmgJED4dV92kxu08duyAtKUkEHqIzQjTU0L3rC3YzQDyqEgtKKn6CylHjKxpWyG1OprY6JbGz_KAUuvsZ_WuaBylsZJ73CwOG2kMjmVowseSxftED6xdmmMrpt-ipPXJuK1UzG8R7l14w6r4LXbN8_RiZVDMhe_cY5e71Yvy4fi6fn-cXn7VCjKYCw4YSBJY5kxi66rNZdKU0vBMm4t0QvS6KarwUqmKDGN4hXQSraNZhygBUnn6OqwdxPDx2TSKPowRZ9PiopU7aKibUvyFD9M5VdTisaKTdYv404QEHtDRS_-DBV7QwVkkDoTbw5EkzVsnYkiKWe8MtpFo0ahg_tvxTeVtoUb</recordid><startdate>20181015</startdate><enddate>20181015</enddate><creator>Wang, Congcong</creator><creator>Liu, Junjie</creator><creator>Shang, Wenjin</creator><creator>Sun, Hejiang</creator><creator>Li, Jiayu</creator><creator>Fan, Fenghua</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7ST</scope><scope>8FD</scope><scope>C1K</scope><scope>F28</scope><scope>FR3</scope><scope>KR7</scope><scope>SOI</scope><orcidid>https://orcid.org/0000-0001-6895-5522</orcidid><orcidid>https://orcid.org/0000-0002-5398-1151</orcidid></search><sort><creationdate>20181015</creationdate><title>Experimental and numerical study of space station airflow distribution under microgravity condition</title><author>Wang, Congcong ; Liu, Junjie ; Shang, Wenjin ; Sun, Hejiang ; Li, Jiayu ; Fan, Fenghua</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c340t-6140a18f4ee5bb7d6acd3f30f46ff1d518d8b70fa4c31e8c62032a98d460090a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Aerodynamics</topic><topic>Air flow</topic><topic>Air quality</topic><topic>CFD</topic><topic>Computational fluid dynamics</topic><topic>Computer applications</topic><topic>Contaminants</topic><topic>Convection</topic><topic>Fluid dynamics</topic><topic>Fluid flow</topic><topic>Free convection</topic><topic>Hydrodynamics</topic><topic>K-epsilon turbulence model</topic><topic>Microgravity</topic><topic>Numerical analysis</topic><topic>Particle image velocimetry</topic><topic>Pollutant removal</topic><topic>Scale models</topic><topic>Shrinkable ratio method</topic><topic>Space stations</topic><topic>Thermal comfort</topic><topic>Thermal energy</topic><topic>Turbulence</topic><topic>Turbulence models</topic><topic>Velocity distribution</topic><topic>Velocity measurement</topic><topic>Weightlessness</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wang, Congcong</creatorcontrib><creatorcontrib>Liu, Junjie</creatorcontrib><creatorcontrib>Shang, Wenjin</creatorcontrib><creatorcontrib>Sun, Hejiang</creatorcontrib><creatorcontrib>Li, Jiayu</creatorcontrib><creatorcontrib>Fan, Fenghua</creatorcontrib><collection>CrossRef</collection><collection>Environment Abstracts</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><collection>Environment Abstracts</collection><jtitle>Building and environment</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wang, Congcong</au><au>Liu, Junjie</au><au>Shang, Wenjin</au><au>Sun, Hejiang</au><au>Li, Jiayu</au><au>Fan, Fenghua</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental and numerical study of space station airflow distribution under microgravity condition</atitle><jtitle>Building and environment</jtitle><date>2018-10-15</date><risdate>2018</risdate><volume>144</volume><spage>268</spage><epage>280</epage><pages>268-280</pages><issn>0360-1323</issn><eissn>1873-684X</eissn><abstract>A space station that operates under microgravity conditions is a closed environment where a reasonable airflow distribution is required to eliminate body heat dissipation, remove contaminants and thus keep the crew comfortable. However, design of a reasonable airflow distribution has remained challenging. In this study, a computational fluid dynamics (CFD) methods with various turbulence models were used to investigate the airflow distribution inside a space station under microgravity conditions. To compare the performance of different models, the shrinkable ratio method was used to set up a mockup station to eliminate the influence of gravity-induced natural convection. The air velocity distribution in the narrow scale model was measured using particle image velocimetry (PIV). Results showed that the performance of the standard k-ε turbulence model was better than the renormalized group (RNG) k-ε turbulence model. The air distribution was optimized by changing the angle of the air supply outlet, suggesting that a three-dimensional air supply can provide better thermal comfort and higher air quality.
•CFD method was used to study the airflow distribution in enclosure under microgravity conditions.•Shrinkable ratio method was used to eliminate the influence of natural convection on airflow at ground test.•Airflow in the shrinkable ratio model was measured using PIV technique.•Three-dimensional air supply can provide more reasonable velocity distribution than vertical air supply.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.buildenv.2018.08.017</doi><tpages>13</tpages><orcidid>https://orcid.org/0000-0001-6895-5522</orcidid><orcidid>https://orcid.org/0000-0002-5398-1151</orcidid></addata></record> |
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subjects | Aerodynamics Air flow Air quality CFD Computational fluid dynamics Computer applications Contaminants Convection Fluid dynamics Fluid flow Free convection Hydrodynamics K-epsilon turbulence model Microgravity Numerical analysis Particle image velocimetry Pollutant removal Scale models Shrinkable ratio method Space stations Thermal comfort Thermal energy Turbulence Turbulence models Velocity distribution Velocity measurement Weightlessness |
title | Experimental and numerical study of space station airflow distribution under microgravity condition |
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