For the laminar thermal boundary layer over a flat plate with uniform heat flux, develop the similarity solution with q"=constant (see Ref. 27). As a similarity temperature variable, choose 0(n, Pr), where T-T, 8. (q"/k)(1x/U)"2 Where n is defined in the Blasius solution. Based on the same approach for Blasius solution, show that the energy equation in the boundary layer reduces to, Pr O"+(fe -fe) 2 Where f is the solution from Blasius solution. Ue, Te, P T Solid wall