Characterization of arcjet flows using laser-induced fluorescence
A sensor based on laser-induced fluorescence has been installed at the 20-MW NASA Ames Aerodynamic Heating Facility. The sensor has provided new, quantitative, real-time information about properties of the arcjet flow in the highly dissociated, partially ionized, nonequilibrium regime. Number densit...
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Veröffentlicht in: | Journal of thermophysics and heat transfer 1995-01, Vol.9 (1), p.26-33 |
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creator | Bamford, Douglas J O'Keefe, Anthony Babikian, Dikran S Stewart, David A Strawa, Anthony W |
description | A sensor based on laser-induced fluorescence has been installed at the 20-MW NASA Ames Aerodynamic Heating Facility. The sensor has provided new, quantitative, real-time information about properties of the arcjet flow in the highly dissociated, partially ionized, nonequilibrium regime. Number densities of atomic oxygen, flow velocities, heavy particle translational temperatures, and collisional quenching rates have been measured. These results have been used to test and refine computational models of the arcjet flow. The calculated number densities, translational temperatures, and flow velocities are in moderately good agreement with experiment. (Author) |
doi_str_mv | 10.2514/3.624 |
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The sensor has provided new, quantitative, real-time information about properties of the arcjet flow in the highly dissociated, partially ionized, nonequilibrium regime. Number densities of atomic oxygen, flow velocities, heavy particle translational temperatures, and collisional quenching rates have been measured. These results have been used to test and refine computational models of the arcjet flow. The calculated number densities, translational temperatures, and flow velocities are in moderately good agreement with experiment. (Author)</description><identifier>ISSN: 0887-8722</identifier><identifier>EISSN: 1533-6808</identifier><identifier>DOI: 10.2514/3.624</identifier><identifier>CODEN: JTHTEO</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>Arc jet flow ; Exact sciences and technology ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; Instrumentation for fluid dynamics ; Laser induced fluorescence ; Nonequilibrium gas dynamics ; Physics ; Reactive, radiative, or nonequilibrium flows</subject><ispartof>Journal of thermophysics and heat transfer, 1995-01, Vol.9 (1), p.26-33</ispartof><rights>1995 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Jan 1995</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a432t-9ee422942e9930638a374bc69d898ca144907f95fd9d500e1adb9b44dc213b1c3</citedby><cites>FETCH-LOGICAL-a432t-9ee422942e9930638a374bc69d898ca144907f95fd9d500e1adb9b44dc213b1c3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,310,314,776,780,785,786,4036,4037,23909,23910,25118,27901,27902</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=3385174$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Bamford, Douglas J</creatorcontrib><creatorcontrib>O'Keefe, Anthony</creatorcontrib><creatorcontrib>Babikian, Dikran S</creatorcontrib><creatorcontrib>Stewart, David A</creatorcontrib><creatorcontrib>Strawa, Anthony W</creatorcontrib><title>Characterization of arcjet flows using laser-induced fluorescence</title><title>Journal of thermophysics and heat transfer</title><description>A sensor based on laser-induced fluorescence has been installed at the 20-MW NASA Ames Aerodynamic Heating Facility. The sensor has provided new, quantitative, real-time information about properties of the arcjet flow in the highly dissociated, partially ionized, nonequilibrium regime. Number densities of atomic oxygen, flow velocities, heavy particle translational temperatures, and collisional quenching rates have been measured. These results have been used to test and refine computational models of the arcjet flow. The calculated number densities, translational temperatures, and flow velocities are in moderately good agreement with experiment. (Author)</description><subject>Arc jet flow</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Instrumentation for fluid dynamics</subject><subject>Laser induced fluorescence</subject><subject>Nonequilibrium gas dynamics</subject><subject>Physics</subject><subject>Reactive, radiative, or nonequilibrium flows</subject><issn>0887-8722</issn><issn>1533-6808</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1995</creationdate><recordtype>article</recordtype><recordid>eNpt0MlOwzAQBmALgUQpfYeI9ZTiLYl9rCo2CYkLnK2JY4OrNC52Ipanx6UVCMRpDvPp_0eD0ITgKS0Iv2DTkvIdNCIFY3kpsNhFIyxElYuK0n10EOMCY1KKiozQbP4MAXRvgvuA3vku8zaDoBemz2zrX2M2RNc9ZS1EE3LXNYM2TdoMPpioTafNIdqz0EYz2c4xery6fJjf5Hf317fz2V0OnNE-l8ZwSiWnRkqGSyaAVbzWpWyEFBoI5xJXVha2kU2BsSHQ1LLmvNGUsJpoNkZnm9xV8C-Dib1aunRB20Jn_BAVrRiRjIkEj__AhR9Cl25TlBEiJSYEJ3W6UTr4GIOxahXcEsK7Ilit36iYSm9M7mSbBlFDawN02sVvnAoLUq3Z-YaBA_gp_MpQq8YqO7Rtb976JI_-k79bPwEF34iZ</recordid><startdate>199501</startdate><enddate>199501</enddate><creator>Bamford, Douglas J</creator><creator>O'Keefe, Anthony</creator><creator>Babikian, Dikran S</creator><creator>Stewart, David A</creator><creator>Strawa, Anthony W</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KR7</scope><scope>L7M</scope></search><sort><creationdate>199501</creationdate><title>Characterization of arcjet flows using laser-induced fluorescence</title><author>Bamford, Douglas J ; O'Keefe, Anthony ; Babikian, Dikran S ; Stewart, David A ; Strawa, Anthony W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a432t-9ee422942e9930638a374bc69d898ca144907f95fd9d500e1adb9b44dc213b1c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1995</creationdate><topic>Arc jet flow</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Instrumentation for fluid dynamics</topic><topic>Laser induced fluorescence</topic><topic>Nonequilibrium gas dynamics</topic><topic>Physics</topic><topic>Reactive, radiative, or nonequilibrium flows</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bamford, Douglas J</creatorcontrib><creatorcontrib>O'Keefe, Anthony</creatorcontrib><creatorcontrib>Babikian, Dikran S</creatorcontrib><creatorcontrib>Stewart, David A</creatorcontrib><creatorcontrib>Strawa, Anthony W</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of thermophysics and heat transfer</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bamford, Douglas J</au><au>O'Keefe, Anthony</au><au>Babikian, Dikran S</au><au>Stewart, David A</au><au>Strawa, Anthony W</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Characterization of arcjet flows using laser-induced fluorescence</atitle><jtitle>Journal of thermophysics and heat transfer</jtitle><date>1995-01</date><risdate>1995</risdate><volume>9</volume><issue>1</issue><spage>26</spage><epage>33</epage><pages>26-33</pages><issn>0887-8722</issn><eissn>1533-6808</eissn><coden>JTHTEO</coden><abstract>A sensor based on laser-induced fluorescence has been installed at the 20-MW NASA Ames Aerodynamic Heating Facility. The sensor has provided new, quantitative, real-time information about properties of the arcjet flow in the highly dissociated, partially ionized, nonequilibrium regime. Number densities of atomic oxygen, flow velocities, heavy particle translational temperatures, and collisional quenching rates have been measured. These results have been used to test and refine computational models of the arcjet flow. The calculated number densities, translational temperatures, and flow velocities are in moderately good agreement with experiment. (Author)</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.624</doi><tpages>8</tpages></addata></record> |
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subjects | Arc jet flow Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Instrumentation for fluid dynamics Laser induced fluorescence Nonequilibrium gas dynamics Physics Reactive, radiative, or nonequilibrium flows |
title | Characterization of arcjet flows using laser-induced fluorescence |
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