Engineering, 12.03.2020 03:09 joaquin42
Consider a flat plate with the surf-ace heat flux specified as ,, l2O W/m2 when 0 { x { 15 cm, 4,, : ll0 W/m2 when x ) 15 cm. Air at atmospheric pressure and 20"C flows over this plate at 3 m/s. Estimate the variation of wall temperature with the distance x fiom the leading edge in the laminar boundary layer region, and evaluate the wall temperature numerically at 30 cm.
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Consider a flat plate with the surf-ace heat flux specified as ,, l2O W/m2 when 0 { x { 15 cm, 4,, :...
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