The similarity solutions for the governing ordinary differential equat
ions of the boundary layer corresponding to a stretching surface have
been reported. Power law velocity and temperature distribution were as
sumed for velocity exponent 3 greater-than-or-equal-to m greater-than-
or-equal-to - 0.41176, - 1.1 greater-than-or-equal-to m greater-than-o
r-equal-to - 3, and for temperature exponent 3 greater-than-or-equal-t
o n greater-than-or-equal-to - 3. Solutions have been found for n = 0
and all m where heat transferred from the stretching surface to the am
bient. The direction and amount of heat flow were found to be dependen
t on the magnitude of n and m for the same Prandtl number. Nusselt num
ber increases with increasing m and Pr for uniform and variable surfac
e temperature however, for uniform surface heat flux it decreases with
increasing m for constant Pr.