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sciences naturelles et appliquées - iate.europa.eu
Impact pressure and total temperature interpretation at hypersonic mach numbers...number.Temperature recovery factors for the total-temperature probe were obtained throughout a Reynolds number range from 30,800 to 213,000, where the Reynolds number was based on the...
général - core.ac.uk - PDF: thesis.library.caltech.edu
Experimental heat transfer at hypersonic mach mumber...6].A flat plate temperature recovery factor of ...
Investigating the influence of helium based mixtures composition on the temperature recovery factor and prandtl number values... For the Leontiev’s tube, using the helium binary gas mixtures with low Pr values results in significant drop of the temperature recovery factor r value on the wall in supersonic flow and in rise of the available temperature difference with appropriate increase of heat flow densities and decrease...
 PDF: doaj.org
Heat transfer on an afterbody immersed in the separated wake of a hemisphere /Tests were conducted to determine the average heat transfer and temperature recovery factor on a tapered cylindrical afterbody immersed in the wake of a hemisphere....

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sciences naturelles et appliquées - iate.europa.eu
sciences naturelles et appliquées - iate.europa.eu
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