Документ взят из кэша поисковой машины. Адрес оригинального документа : http://termogaz.imec.msu.ru/scientific%20results/supersonic%20dimple/supersonic%20dimples_e.htm
Дата изменения: Mon Mar 30 10:11:29 2009
Дата индексирования: Mon Oct 1 19:39:33 2012
Кодировка: Windows-1251
Поисковые слова: shadow
supersonic dimples_e
Heat transfer intensification on surfaces with 'eddy generating' relief at supersonic velocity of incident flow
The photo of the experimental model: a plate with smooth and 'eddy generating' relief (dimples made as spherical segments).
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The photo of the experimental model: a plate with smooth and 'eddy generating' relief (projections made as spherical segments).
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Shadow photos of flowing over the 'eddy generating' surfaces with dimples and projections made as spherical segments.
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Temperature field on plates with 'eddy generating' relief (dimples and projections) М=3.1
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Local coefficients of heat transfer distribution on plates with 'eddy generating' relief (dimples and projections) and a smooth plate flown over by supersonic air stream M=3
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Experimental unit for measuring coefficients of heat transfer and pressure drop on plates with 'eddy generating' relief and a smooth plate flown over by supersonic air stream, these plates are mounted inside the aerodynamic tube A-11
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Experimental unit for measuring coefficients of heat transfer and pressure drop on plates with 'eddy generating' relief and a smooth plate flown over by supersonic air stream, these plates are mounted inside the aerodynamic tube A-11
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Temperature distribution during flowing of supersonic stream over a single dimple
Temperature distribution during flowing of supersonic stream over a single dimple (maximum temperatures correspond with the centre of a dimple)
Temperature distribution during flowing of supersonic stream over the cylindrical bar (stream flow direction - from the bottom to the top)
Temperature distribution during flowing of supersonic stream over the dimpled cylindrical bar (stream flow direction - from the bottom to the top)
Temperature distribution during flowing of supersonic stream over the cylindrical bar with circular rectangular grooves (stream flow direction - from the bottom to the top)
Temperature distribution during flowing of supersonic stream over a cylindrical bar with corrugation surface (stream flow direction - from bottom to top)