Physics, 30.03.2020 18:57 aaliyahnv07
In a particular application involving airflow over a surface, the boundary layer temperature distribution may be approximated as T−Ts/T[infinity]−Ts=1−exp(−Pr(u[in finity]y)/) Where y is the distance normal to the surface and the Prandtl number, Pr=cpμ/k=0.7, is a dimensionless fluid property. If T[infinity]=400K, Ts=300K, and u[infinity]/υ=5000 m-1, what is the surface heat flux? 6.11
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