In a particular application involving airflow over a surface, the boundary layer temperature distribution may be approximated as TTsT(y)Ts=1exp(Prvuy) where y is the distance normal to the surface and the PrandtI number, Pr=cp/k=0.7, is a dimensionless fluid property. If T=400K,Ts=300K, and u/v=5000m1, what is the surface heat flux in the y-direction, in W/m2 ? qs=W/m2 eTextbook and Media Attempts: unlimited