Turbulent flow in supersonic and hypersonic nozzles
The calculated turbulent flow properties in a supersonic or a hypersonic wind tunnel nozzle are affected by the location of laminar-turbulent transition point and the behavior of the particular turbulence models considered. A study numerically examined these effects by solving Reynolds-averaged Navi...
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| Veröffentlicht in: | AIAA journal 1995-09, Vol.33 (9), p.1634-1640 |
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| container_end_page | 1640 |
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| container_title | AIAA journal |
| container_volume | 33 |
| creator | Hu, Jiasen Rizzi, Arthur |
| description | The calculated turbulent flow properties in a supersonic or a hypersonic wind tunnel nozzle are affected by the location of laminar-turbulent transition point and the behavior of the particular turbulence models considered. A study numerically examined these effects by solving Reynolds-averaged Navier-Stokes equations for two nozzles. |
| doi_str_mv | 10.2514/3.12861 |
| format | Article |
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A study numerically examined these effects by solving Reynolds-averaged Navier-Stokes equations for two nozzles.</description><subject>Aircraft</subject><subject>Compressible flows; shock and detonation phenomena</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Supersonic and hypersonic flows</subject><subject>Turbulence</subject><subject>Wind tunnels</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1995</creationdate><recordtype>article</recordtype><recordid>eNpt0F1LwzAUBuAgCs4p_oUionjR2ZOPNb2U4RcMvJngXThNE-zI2pq06Pbr7dyYol6FQx7ec3gJOYVkRAXwazYCKsewRwYgGIuZFC_7ZJAkCcTABT0kRyHM-4mmEgaEzTqfd85UbWRd_R6VVRS6xvhQV6WOsCqi1-VurOrVyplwTA4sumBOtu-QPN_dziYP8fTp_nFyM42RpayNudaU04JaC8bkBYMCqJYCJVguIesvyFKRcgoWjRU6z3Km0bAiK9AioGZDcrHJbXz91pnQqkUZtHEOK1N3QdFxIiRnWQ_PfsF53fmqv03RdQlcMujR5QZpX4fgjVWNLxfolwoStW5OMfXVXC_Pt3EYNDrrsdJl2HE2FpD-ZFgifm_8m3b1H9t-q6awynbOteajZZ_LYYY_</recordid><startdate>19950901</startdate><enddate>19950901</enddate><creator>Hu, Jiasen</creator><creator>Rizzi, Arthur</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>L7M</scope></search><sort><creationdate>19950901</creationdate><title>Turbulent flow in supersonic and hypersonic nozzles</title><author>Hu, Jiasen ; Rizzi, Arthur</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a373t-4cc242d2ff1eebd31d12c85a81f48190129757421faef5cb9b3cae3d9dafa1ac3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1995</creationdate><topic>Aircraft</topic><topic>Compressible flows; shock and detonation phenomena</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Supersonic and hypersonic flows</topic><topic>Turbulence</topic><topic>Wind tunnels</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hu, Jiasen</creatorcontrib><creatorcontrib>Rizzi, Arthur</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>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hu, Jiasen</au><au>Rizzi, Arthur</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Turbulent flow in supersonic and hypersonic nozzles</atitle><jtitle>AIAA journal</jtitle><date>1995-09-01</date><risdate>1995</risdate><volume>33</volume><issue>9</issue><spage>1634</spage><epage>1640</epage><pages>1634-1640</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>The calculated turbulent flow properties in a supersonic or a hypersonic wind tunnel nozzle are affected by the location of laminar-turbulent transition point and the behavior of the particular turbulence models considered. 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| fulltext | fulltext |
| identifier | ISSN: 0001-1452 |
| ispartof | AIAA journal, 1995-09, Vol.33 (9), p.1634-1640 |
| issn | 0001-1452 1533-385X |
| language | eng |
| recordid | cdi_aiaa_journals_3_12861_pdf_fulltext |
| source | Alma/SFX Local Collection |
| subjects | Aircraft Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Supersonic and hypersonic flows Turbulence Wind tunnels |
| title | Turbulent flow in supersonic and hypersonic nozzles |
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