MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY
The report describes the experimental measurement of aerodynamic heat transfer to a two-dimensional variable geometry hypersonic inlet model. The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,0...
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| creator | Tabakoff,Widen mcDonel,James D |
| description | The report describes the experimental measurement of aerodynamic heat transfer to a two-dimensional variable geometry hypersonic inlet model. The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,000 and 631,000 per foot. The experimental results are compared to an approximate theoretical solution for laminar boundary layer flow over a flat plate. (Author) |
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The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,000 and 631,000 per foot. The experimental results are compared to an approximate theoretical solution for laminar boundary layer flow over a flat plate. (Author)</description><language>eng</language><subject>DUCT INLETS ; Fluid Mechanics ; GEOMETRIC FORMS ; HEAT TRANSFER ; HYPERSONIC FLOW ; LAMINAR BOUNDARY LAYER ; MEASUREMENT ; Thermodynamics ; TWO DIMENSIONAL</subject><creationdate>1965</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>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0625095$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Tabakoff,Widen</creatorcontrib><creatorcontrib>mcDonel,James D</creatorcontrib><creatorcontrib>CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING</creatorcontrib><title>MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY</title><description>The report describes the experimental measurement of aerodynamic heat transfer to a two-dimensional variable geometry hypersonic inlet model. The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,000 and 631,000 per foot. The experimental results are compared to an approximate theoretical solution for laminar boundary layer flow over a flat plate. (Author)</description><subject>DUCT INLETS</subject><subject>Fluid Mechanics</subject><subject>GEOMETRIC FORMS</subject><subject>HEAT TRANSFER</subject><subject>HYPERSONIC FLOW</subject><subject>LAMINAR BOUNDARY LAYER</subject><subject>MEASUREMENT</subject><subject>Thermodynamics</subject><subject>TWO DIMENSIONAL</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1965</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFyrEKwjAQgOEsDqK-gcO9QKEoFRzP9mICSU6S09JBimiFgrg0748O7k7_8P1zdfWE6RzJUxBgDWIIDKGARAxJUwRhQJCWi8Z-p2Q5oAPTnSgmDrYGGxwJtFYMXDBaPDiCI7Enid1SzZ631zSsfl2otSapTfHI472f8vgeco9NudtU5b7a_uEP9qYvww</recordid><startdate>196511</startdate><enddate>196511</enddate><creator>Tabakoff,Widen</creator><creator>mcDonel,James D</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>196511</creationdate><title>MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY</title><author>Tabakoff,Widen ; mcDonel,James D</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06250953</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1965</creationdate><topic>DUCT INLETS</topic><topic>Fluid Mechanics</topic><topic>GEOMETRIC FORMS</topic><topic>HEAT TRANSFER</topic><topic>HYPERSONIC FLOW</topic><topic>LAMINAR BOUNDARY LAYER</topic><topic>MEASUREMENT</topic><topic>Thermodynamics</topic><topic>TWO DIMENSIONAL</topic><toplevel>online_resources</toplevel><creatorcontrib>Tabakoff,Widen</creatorcontrib><creatorcontrib>mcDonel,James D</creatorcontrib><creatorcontrib>CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Tabakoff,Widen</au><au>mcDonel,James D</au><aucorp>CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY</btitle><date>1965-11</date><risdate>1965</risdate><abstract>The report describes the experimental measurement of aerodynamic heat transfer to a two-dimensional variable geometry hypersonic inlet model. The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,000 and 631,000 per foot. The experimental results are compared to an approximate theoretical solution for laminar boundary layer flow over a flat plate. (Author)</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| source | DTIC Technical Reports |
| subjects | DUCT INLETS Fluid Mechanics GEOMETRIC FORMS HEAT TRANSFER HYPERSONIC FLOW LAMINAR BOUNDARY LAYER MEASUREMENT Thermodynamics TWO DIMENSIONAL |
| title | MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY |
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