Microwave Shock-Speed Diagnostic Development and Analysis of Expansion Tunnel Viscous Effects
The development of a nonintrusive microwave shock-speed measurement for expansion tunnels is presented, based on microwave standing-wave reflection. Testing is performed in a large-scale expansion-tunnel facility, with the goal of characterizing viscous effects. Expansion tunnels generate high-entha...
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description | The development of a nonintrusive microwave shock-speed measurement for expansion tunnels is presented, based on microwave standing-wave reflection. Testing is performed in a large-scale expansion-tunnel facility, with the goal of characterizing viscous effects. Expansion tunnels generate high-enthalpy test conditions for short test times, and the test gas is never heated such that excessive freestream dissociation or ionization occurs. The microwave system measures primary and secondary shock speeds accurately and with high spatial resolution along the length of the facility, yielding more accurate freestream conditions. It is shown to be both practical and low cost. The high spatial resolution along the tunnel is used to assess shock-speed attenuation. Negligible shock attenuation is found over a wide range of test conditions and gases, attributed to the large diameter of the facility’s driven and expansion tubes. Shock-tube boundary-layer growth solutions based on Mirels’s theory (“Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer,” AIAA Journal, Vol. 2, No. 1, 1964, pp. 84–93) and a Pitot-probe survey confirm that, in the current facility, the test conditions should not be adversely affected by viscous effects. Mirels’s theory is also used to determine the displacement thicknesses for quasi-one-dimensional analyses, showing how viscous effects become significant in long, smaller-diameter facilities. The high spatial resolution allows for local shock-speed information to evaluate nonideal secondary-diaphragm ruptures. Additionally, when postshock electron-density levels are near the cutoff required for standing-wave reflection, test-gas velocities are measured rather than shock velocities. |
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Testing is performed in a large-scale expansion-tunnel facility, with the goal of characterizing viscous effects. Expansion tunnels generate high-enthalpy test conditions for short test times, and the test gas is never heated such that excessive freestream dissociation or ionization occurs. The microwave system measures primary and secondary shock speeds accurately and with high spatial resolution along the length of the facility, yielding more accurate freestream conditions. It is shown to be both practical and low cost. The high spatial resolution along the tunnel is used to assess shock-speed attenuation. Negligible shock attenuation is found over a wide range of test conditions and gases, attributed to the large diameter of the facility’s driven and expansion tubes. Shock-tube boundary-layer growth solutions based on Mirels’s theory (“Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer,” AIAA Journal, Vol. 2, No. 1, 1964, pp. 84–93) and a Pitot-probe survey confirm that, in the current facility, the test conditions should not be adversely affected by viscous effects. Mirels’s theory is also used to determine the displacement thicknesses for quasi-one-dimensional analyses, showing how viscous effects become significant in long, smaller-diameter facilities. The high spatial resolution allows for local shock-speed information to evaluate nonideal secondary-diaphragm ruptures. Additionally, when postshock electron-density levels are near the cutoff required for standing-wave reflection, test-gas velocities are measured rather than shock velocities.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J053139</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Attenuation ; Diagnostic systems ; Diameters ; Dimensional analysis ; Enthalpy ; Expansion tubes ; Ionization ; Microwaves ; Reflection ; Spatial resolution ; Standing waves ; Test times ; Testing time ; Tunnels ; Tunnels (transportation) ; Turbulent boundary layer ; Velocity ; Viscosity ; Wave reflection</subject><ispartof>AIAA journal, 2015-03, Vol.53 (3), p.573-587</ispartof><rights>Copyright © 2014 by Matthew J. Ringuette, Aaron T. Dufrene, and Michael S. Holden. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code and $10.00 in correspondence with the CCC.</rights><rights>Copyright © 2014 by Matthew J. Ringuette, Aaron T. Dufrene, and Michael S. Holden. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code 1533-385X/15 and $10.00 in correspondence with the CCC.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a349t-5ca5dd780b5ce982282ecbf1d23220376aaf00097d301cce40f2b07fa995c5163</citedby><cites>FETCH-LOGICAL-a349t-5ca5dd780b5ce982282ecbf1d23220376aaf00097d301cce40f2b07fa995c5163</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27923,27924</link.rule.ids></links><search><creatorcontrib>Dufrene, Aaron T</creatorcontrib><creatorcontrib>Holden, Michael S</creatorcontrib><creatorcontrib>Ringuette, Matthew J</creatorcontrib><title>Microwave Shock-Speed Diagnostic Development and Analysis of Expansion Tunnel Viscous Effects</title><title>AIAA journal</title><description>The development of a nonintrusive microwave shock-speed measurement for expansion tunnels is presented, based on microwave standing-wave reflection. Testing is performed in a large-scale expansion-tunnel facility, with the goal of characterizing viscous effects. Expansion tunnels generate high-enthalpy test conditions for short test times, and the test gas is never heated such that excessive freestream dissociation or ionization occurs. The microwave system measures primary and secondary shock speeds accurately and with high spatial resolution along the length of the facility, yielding more accurate freestream conditions. It is shown to be both practical and low cost. The high spatial resolution along the tunnel is used to assess shock-speed attenuation. Negligible shock attenuation is found over a wide range of test conditions and gases, attributed to the large diameter of the facility’s driven and expansion tubes. Shock-tube boundary-layer growth solutions based on Mirels’s theory (“Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer,” AIAA Journal, Vol. 2, No. 1, 1964, pp. 84–93) and a Pitot-probe survey confirm that, in the current facility, the test conditions should not be adversely affected by viscous effects. Mirels’s theory is also used to determine the displacement thicknesses for quasi-one-dimensional analyses, showing how viscous effects become significant in long, smaller-diameter facilities. The high spatial resolution allows for local shock-speed information to evaluate nonideal secondary-diaphragm ruptures. Additionally, when postshock electron-density levels are near the cutoff required for standing-wave reflection, test-gas velocities are measured rather than shock velocities.</description><subject>Aerodynamics</subject><subject>Attenuation</subject><subject>Diagnostic systems</subject><subject>Diameters</subject><subject>Dimensional analysis</subject><subject>Enthalpy</subject><subject>Expansion tubes</subject><subject>Ionization</subject><subject>Microwaves</subject><subject>Reflection</subject><subject>Spatial resolution</subject><subject>Standing waves</subject><subject>Test times</subject><subject>Testing time</subject><subject>Tunnels</subject><subject>Tunnels (transportation)</subject><subject>Turbulent boundary layer</subject><subject>Velocity</subject><subject>Viscosity</subject><subject>Wave reflection</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><recordid>eNp90U1LwzAYB_AgCs7pwW8QEEQPnXmSpm2OY5tvTDxsihcJWZpoZ5fUppvu21vZDqLg6eGBH3-eF4SOgfQoh_gCereEM2BiB3WAMxaxjD_tog4hBCKIOd1HByHM246mGXTQ812ha_-hVgZPXr1-iyaVMTkeFurF-dAUGg_NypS-WhjXYOVy3HeqXIciYG_x6LNSLhTe4enSOVPixyJovwx4ZK3RTThEe1aVwRxtaxc9XI6mg-tofH91M-iPI8Vi0URcK57naUZmXBuRUZpRo2cWcsooJSxNlLLtAiLNGQGtTUwsnZHUKiG45pCwLjrb5Fa1f1-a0MhFO4gpS-VMO46EJBFZklCIW3ryi879sm53CpLGAhhJBaT_KUh4LNKtOt-o9oQh1MbKqi4Wql5LIPL7HRLk9h2tPd1YVSj1I-0P_AKceIaz</recordid><startdate>201503</startdate><enddate>201503</enddate><creator>Dufrene, Aaron T</creator><creator>Holden, Michael S</creator><creator>Ringuette, Matthew J</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>201503</creationdate><title>Microwave Shock-Speed Diagnostic Development and Analysis of Expansion Tunnel Viscous Effects</title><author>Dufrene, Aaron T ; Holden, Michael S ; Ringuette, Matthew J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a349t-5ca5dd780b5ce982282ecbf1d23220376aaf00097d301cce40f2b07fa995c5163</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Aerodynamics</topic><topic>Attenuation</topic><topic>Diagnostic systems</topic><topic>Diameters</topic><topic>Dimensional analysis</topic><topic>Enthalpy</topic><topic>Expansion tubes</topic><topic>Ionization</topic><topic>Microwaves</topic><topic>Reflection</topic><topic>Spatial resolution</topic><topic>Standing waves</topic><topic>Test times</topic><topic>Testing time</topic><topic>Tunnels</topic><topic>Tunnels (transportation)</topic><topic>Turbulent boundary layer</topic><topic>Velocity</topic><topic>Viscosity</topic><topic>Wave reflection</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Dufrene, Aaron T</creatorcontrib><creatorcontrib>Holden, Michael S</creatorcontrib><creatorcontrib>Ringuette, Matthew J</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>Dufrene, Aaron T</au><au>Holden, Michael S</au><au>Ringuette, Matthew J</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Microwave Shock-Speed Diagnostic Development and Analysis of Expansion Tunnel Viscous Effects</atitle><jtitle>AIAA journal</jtitle><date>2015-03</date><risdate>2015</risdate><volume>53</volume><issue>3</issue><spage>573</spage><epage>587</epage><pages>573-587</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>The development of a nonintrusive microwave shock-speed measurement for expansion tunnels is presented, based on microwave standing-wave reflection. Testing is performed in a large-scale expansion-tunnel facility, with the goal of characterizing viscous effects. Expansion tunnels generate high-enthalpy test conditions for short test times, and the test gas is never heated such that excessive freestream dissociation or ionization occurs. The microwave system measures primary and secondary shock speeds accurately and with high spatial resolution along the length of the facility, yielding more accurate freestream conditions. It is shown to be both practical and low cost. The high spatial resolution along the tunnel is used to assess shock-speed attenuation. Negligible shock attenuation is found over a wide range of test conditions and gases, attributed to the large diameter of the facility’s driven and expansion tubes. Shock-tube boundary-layer growth solutions based on Mirels’s theory (“Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer,” AIAA Journal, Vol. 2, No. 1, 1964, pp. 84–93) and a Pitot-probe survey confirm that, in the current facility, the test conditions should not be adversely affected by viscous effects. Mirels’s theory is also used to determine the displacement thicknesses for quasi-one-dimensional analyses, showing how viscous effects become significant in long, smaller-diameter facilities. The high spatial resolution allows for local shock-speed information to evaluate nonideal secondary-diaphragm ruptures. Additionally, when postshock electron-density levels are near the cutoff required for standing-wave reflection, test-gas velocities are measured rather than shock velocities.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J053139</doi><tpages>15</tpages></addata></record> |
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subjects | Aerodynamics Attenuation Diagnostic systems Diameters Dimensional analysis Enthalpy Expansion tubes Ionization Microwaves Reflection Spatial resolution Standing waves Test times Testing time Tunnels Tunnels (transportation) Turbulent boundary layer Velocity Viscosity Wave reflection |
title | Microwave Shock-Speed Diagnostic Development and Analysis of Expansion Tunnel Viscous Effects |
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