摘要: Abstract The traditional laminar plane wall jet is studied when the medium filled with nanoparticles of Ag, Cu, CuO, Al2O3 and TiO2. It aimed to understand effects several nanofluids on heat flow behaviors jet. Momentum thermal integral flux relations are obtained initially. Later on, some important shape factors defined designing momentum boundary layer, shear layer as well subjected either adiabatic or isothermal constraints. By means these parameters, field shown be decelerated a consequence stress enhanced. Without solving energy equation, factor enables one fully seize cooling effect considered for both cases. As result, transfer rate found greatly enhanced by presence nanoparticles. Same conclusions reached two different popular nanofluid models made use in recent researches.
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