MEASUREMENTS OF FREE MOLECULE HEAT TRANSFER IN AIR AT MACH NUMBERS FROM 10-18

Heat transfer measurements to fine wires in the freemolecule flow regime at Mach numbers typical of the conditions in which satellites move were made. Accommodation coefficients obtained within the accuracy of these experiments agree with those obtained at much lower Mach numbers. The heat transfer...

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description Heat transfer measurements to fine wires in the freemolecule flow regime at Mach numbers typical of the conditions in which satellites move were made. Accommodation coefficients obtained within the accuracy of these experiments agree with those obtained at much lower Mach numbers. The heat transfer measurements taken indicate no Mach number effect. At high Reynolds numbers, where free-molecule flow is no longer obtained, agreement with previous data is reasonable down to Knudsen number equal to one, corresponding to Reynolds number of 5 or less. A further decrease in the Knudsen number concomitant with an increase in the Reynolds number yields heat transfer rates that are somewhat lower, although in essential agreement, with previously acquired data. With an appropriate calibration for the degree of rarefaction of the gas, a wire probe shows promise as a fast reacting instrument for use in gas flows of quite low density. (Author)
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Accommodation coefficients obtained within the accuracy of these experiments agree with those obtained at much lower Mach numbers. The heat transfer measurements taken indicate no Mach number effect. At high Reynolds numbers, where free-molecule flow is no longer obtained, agreement with previous data is reasonable down to Knudsen number equal to one, corresponding to Reynolds number of 5 or less. A further decrease in the Knudsen number concomitant with an increase in the Reynolds number yields heat transfer rates that are somewhat lower, although in essential agreement, with previously acquired data. With an appropriate calibration for the degree of rarefaction of the gas, a wire probe shows promise as a fast reacting instrument for use in gas flows of quite low density. (Author)</description><language>eng</language><subject>ARTIFICIAL SATELLITES ; GAS FLOW ; HEAT TRANSFER ; MEASUREMENT ; RAREFIED GAS DYNAMICS ; REYNOLDS NUMBER ; SHOCK TUBES ; WIRE</subject><creationdate>1960</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/AD0607933$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VARWIG,R L</creatorcontrib><creatorcontrib>TRW SPACE TECHNOLOGY LABS LOS ANGELES CALIF</creatorcontrib><title>MEASUREMENTS OF FREE MOLECULE HEAT TRANSFER IN AIR AT MACH NUMBERS FROM 10-18</title><description>Heat transfer measurements to fine wires in the freemolecule flow regime at Mach numbers typical of the conditions in which satellites move were made. Accommodation coefficients obtained within the accuracy of these experiments agree with those obtained at much lower Mach numbers. The heat transfer measurements taken indicate no Mach number effect. At high Reynolds numbers, where free-molecule flow is no longer obtained, agreement with previous data is reasonable down to Knudsen number equal to one, corresponding to Reynolds number of 5 or less. A further decrease in the Knudsen number concomitant with an increase in the Reynolds number yields heat transfer rates that are somewhat lower, although in essential agreement, with previously acquired data. With an appropriate calibration for the degree of rarefaction of the gas, a wire probe shows promise as a fast reacting instrument for use in gas flows of quite low density. (Author)</description><subject>ARTIFICIAL SATELLITES</subject><subject>GAS FLOW</subject><subject>HEAT TRANSFER</subject><subject>MEASUREMENT</subject><subject>RAREFIED GAS DYNAMICS</subject><subject>REYNOLDS NUMBER</subject><subject>SHOCK TUBES</subject><subject>WIRE</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1960</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZPD1dXUMDg1y9XX1CwlW8HdTcAtydVXw9fdxdQ71cVXwcHUMUQgJcvQLdnMNUvD0U3D0DFIACvk6Onso-IX6OrkGBQO1-PsqGBroGlrwMLCmJeYUp_JCaW4GGTfXEGcP3ZSSzOT44pLMvNSSeEcXAzMDc0tjY2MC0gDJ5ipb</recordid><startdate>19601013</startdate><enddate>19601013</enddate><creator>VARWIG,R L</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19601013</creationdate><title>MEASUREMENTS OF FREE MOLECULE HEAT TRANSFER IN AIR AT MACH NUMBERS FROM 10-18</title><author>VARWIG,R L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06079333</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1960</creationdate><topic>ARTIFICIAL SATELLITES</topic><topic>GAS FLOW</topic><topic>HEAT TRANSFER</topic><topic>MEASUREMENT</topic><topic>RAREFIED GAS DYNAMICS</topic><topic>REYNOLDS NUMBER</topic><topic>SHOCK TUBES</topic><topic>WIRE</topic><toplevel>online_resources</toplevel><creatorcontrib>VARWIG,R L</creatorcontrib><creatorcontrib>TRW SPACE TECHNOLOGY LABS LOS ANGELES CALIF</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>VARWIG,R L</au><aucorp>TRW SPACE TECHNOLOGY LABS LOS ANGELES CALIF</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>MEASUREMENTS OF FREE MOLECULE HEAT TRANSFER IN AIR AT MACH NUMBERS FROM 10-18</btitle><date>1960-10-13</date><risdate>1960</risdate><abstract>Heat transfer measurements to fine wires in the freemolecule flow regime at Mach numbers typical of the conditions in which satellites move were made. Accommodation coefficients obtained within the accuracy of these experiments agree with those obtained at much lower Mach numbers. The heat transfer measurements taken indicate no Mach number effect. At high Reynolds numbers, where free-molecule flow is no longer obtained, agreement with previous data is reasonable down to Knudsen number equal to one, corresponding to Reynolds number of 5 or less. A further decrease in the Knudsen number concomitant with an increase in the Reynolds number yields heat transfer rates that are somewhat lower, although in essential agreement, with previously acquired data. With an appropriate calibration for the degree of rarefaction of the gas, a wire probe shows promise as a fast reacting instrument for use in gas flows of quite low density. (Author)</abstract><oa>free_for_read</oa></addata></record>
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subjects ARTIFICIAL SATELLITES
GAS FLOW
HEAT TRANSFER
MEASUREMENT
RAREFIED GAS DYNAMICS
REYNOLDS NUMBER
SHOCK TUBES
WIRE
title MEASUREMENTS OF FREE MOLECULE HEAT TRANSFER IN AIR AT MACH NUMBERS FROM 10-18
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