2003
DOI: 10.1299/kikaib.69.2305
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Flow and Heat Transfer of Impinging Jet with Low Nozzle-Plate Spacing and Their Control (Effects of Nozzle Wall Thickness and Geometry)

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Cited by 2 publications
(2 citation statements)
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“…T w solid = T wgas , and K w solid ∂T w solid ∂x = K wgas ∂T wgas ∂x (12) No thermal radiation loss from the solid surface is assumed. This is due to the temperature difference within the surface region of the cavity wall.…”
Section: Solid-fluid Interfacementioning
confidence: 99%
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“…T w solid = T wgas , and K w solid ∂T w solid ∂x = K wgas ∂T wgas ∂x (12) No thermal radiation loss from the solid surface is assumed. This is due to the temperature difference within the surface region of the cavity wall.…”
Section: Solid-fluid Interfacementioning
confidence: 99%
“…They showed that the usual method of representing the Nusselt number as a function of Reynolds number was inadequate in the compressible flows where the nozzle Mach number or pressure ratio ought to be included. The flow and heat transfer characteristics during the jet impingement onto a closely spaced plate were examined by Shakouchi et al [12]. They indicated that the heat transfer characteristics could be considerably improved.…”
Section: Introductionmentioning
confidence: 99%