Numerical Analysis of Terminal Double Mach Reflection
Pseudostationary oblique-shock-wave reflections in real and perfect gases were investigated. In particular, we studied the special case of double Mach reflection known as terminal double Mach reflection. Numerical solutions on the inviscid equations are presented and compared with experimental and a...
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| creator | Lijewski,Michael J Glaz,Harland M |
| description | Pseudostationary oblique-shock-wave reflections in real and perfect gases were investigated. In particular, we studied the special case of double Mach reflection known as terminal double Mach reflection. Numerical solutions on the inviscid equations are presented and compared with experimental and analytical results. Disparities between our numerical results and those predicted by the two- and three-shock theory are discussed. Keywords: Euler equations; Mathematical models; Computer codes. (Author) |
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| fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADA179041</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADA179041</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADA1790413</originalsourceid><addsrcrecordid>eNrjZDD1K81NLcpMTsxRcMxLzKkszixWyE9TCEktys0E8hVc8kuTclIVfBOTMxSCUtNyUpNLMvPzeBhY0xJzilN5oTQ3g4yba4izh25KSWZyfHFJZl5qSbyji6OhuaWBiaExAWkAeUQp2A</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Numerical Analysis of Terminal Double Mach Reflection</title><source>DTIC Technical Reports</source><creator>Lijewski,Michael J ; Glaz,Harland M</creator><creatorcontrib>Lijewski,Michael J ; Glaz,Harland M ; NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD</creatorcontrib><description>Pseudostationary oblique-shock-wave reflections in real and perfect gases were investigated. In particular, we studied the special case of double Mach reflection known as terminal double Mach reflection. Numerical solutions on the inviscid equations are presented and compared with experimental and analytical results. Disparities between our numerical results and those predicted by the two- and three-shock theory are discussed. Keywords: Euler equations; Mathematical models; Computer codes. (Author)</description><language>eng</language><subject>COMPUTER PROGRAMS ; DIFFERENTIAL EQUATIONS ; DMR(Double Mach Reflection) ; Euler equations ; Fluid Mechanics ; GASES ; INVISCID FLOW ; MACH NUMBER ; MATHEMATICAL MODELS ; NUMERICAL ANALYSIS ; REFLECTION ; SHOCK WAVES ; SOLUTIONS(GENERAL) ; TDMR(Terminal Double Mach Reflection)</subject><creationdate>1986</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA179041$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Lijewski,Michael J</creatorcontrib><creatorcontrib>Glaz,Harland M</creatorcontrib><creatorcontrib>NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD</creatorcontrib><title>Numerical Analysis of Terminal Double Mach Reflection</title><description>Pseudostationary oblique-shock-wave reflections in real and perfect gases were investigated. In particular, we studied the special case of double Mach reflection known as terminal double Mach reflection. Numerical solutions on the inviscid equations are presented and compared with experimental and analytical results. Disparities between our numerical results and those predicted by the two- and three-shock theory are discussed. Keywords: Euler equations; Mathematical models; Computer codes. (Author)</description><subject>COMPUTER PROGRAMS</subject><subject>DIFFERENTIAL EQUATIONS</subject><subject>DMR(Double Mach Reflection)</subject><subject>Euler equations</subject><subject>Fluid Mechanics</subject><subject>GASES</subject><subject>INVISCID FLOW</subject><subject>MACH NUMBER</subject><subject>MATHEMATICAL MODELS</subject><subject>NUMERICAL ANALYSIS</subject><subject>REFLECTION</subject><subject>SHOCK WAVES</subject><subject>SOLUTIONS(GENERAL)</subject><subject>TDMR(Terminal Double Mach Reflection)</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1986</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZDD1K81NLcpMTsxRcMxLzKkszixWyE9TCEktys0E8hVc8kuTclIVfBOTMxSCUtNyUpNLMvPzeBhY0xJzilN5oTQ3g4yba4izh25KSWZyfHFJZl5qSbyji6OhuaWBiaExAWkAeUQp2A</recordid><startdate>19860826</startdate><enddate>19860826</enddate><creator>Lijewski,Michael J</creator><creator>Glaz,Harland M</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19860826</creationdate><title>Numerical Analysis of Terminal Double Mach Reflection</title><author>Lijewski,Michael J ; Glaz,Harland M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA1790413</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1986</creationdate><topic>COMPUTER PROGRAMS</topic><topic>DIFFERENTIAL EQUATIONS</topic><topic>DMR(Double Mach Reflection)</topic><topic>Euler equations</topic><topic>Fluid Mechanics</topic><topic>GASES</topic><topic>INVISCID FLOW</topic><topic>MACH NUMBER</topic><topic>MATHEMATICAL MODELS</topic><topic>NUMERICAL ANALYSIS</topic><topic>REFLECTION</topic><topic>SHOCK WAVES</topic><topic>SOLUTIONS(GENERAL)</topic><topic>TDMR(Terminal Double Mach Reflection)</topic><toplevel>online_resources</toplevel><creatorcontrib>Lijewski,Michael J</creatorcontrib><creatorcontrib>Glaz,Harland M</creatorcontrib><creatorcontrib>NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Lijewski,Michael J</au><au>Glaz,Harland M</au><aucorp>NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Numerical Analysis of Terminal Double Mach Reflection</btitle><date>1986-08-26</date><risdate>1986</risdate><abstract>Pseudostationary oblique-shock-wave reflections in real and perfect gases were investigated. In particular, we studied the special case of double Mach reflection known as terminal double Mach reflection. Numerical solutions on the inviscid equations are presented and compared with experimental and analytical results. Disparities between our numerical results and those predicted by the two- and three-shock theory are discussed. Keywords: Euler equations; Mathematical models; Computer codes. (Author)</abstract><oa>free_for_read</oa></addata></record> |
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| source | DTIC Technical Reports |
| subjects | COMPUTER PROGRAMS DIFFERENTIAL EQUATIONS DMR(Double Mach Reflection) Euler equations Fluid Mechanics GASES INVISCID FLOW MACH NUMBER MATHEMATICAL MODELS NUMERICAL ANALYSIS REFLECTION SHOCK WAVES SOLUTIONS(GENERAL) TDMR(Terminal Double Mach Reflection) |
| title | Numerical Analysis of Terminal Double Mach Reflection |
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