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Q: In a particular application involving airflow over a heated surface, the boundary layer temperature distribution may be approximated as where y is the distance normal to the surface and the
T-Ts/T∞-Ts = 1-exp(-Pr u∞y/v)
Prandtl number, Pr = cpµ/k = 0.7, is a dimensionless fluid property. If T8 = 400 K. Ts, = 300 K. and u8/v = 5000 m-1, what is the surface heat flux?