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5. The upper surface of a metal plate is being cooled with parallel airflow while its lower surface is subjected to a uniform
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Solin - Given that heat flux = 810 w/m Velocity = 2.5 m/s Temperature =15c find surface Temp at a s1.5m het as assume the surNow = 233209 Cakulate the nusselt number for laminan Plon. Nu - 0.u53 Reyes pola substitute Rex = 233209 and pr=0.7282 Nu = 0Ts=15+810 3.395 s15+239 ITS = 254c) Surface Temperature of the plate at Q=1.5m = 125cc ro

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