Research Abstract
A theoretical study is carried out to investigate the steady laminar
boundary layer
ow due to a rotating frustum of a cone. The symmetry
group and similarity solutions are obtained by employing Lie group the-
ory. The eects of the streamwise coordinate and half cone angle on the
velocity eld are presented.
Keywords: Lie group analysis; Group classication; laminar
ow; boundary
layer; frustum of a cone
Research Department
Research Journal
J. of the Egyptian Mathematical Soc.
Research Member
Research Rank
2
Research Vol
Vol. 15, No.2
Research Year
2007
Research Pages
PP. 233-245