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
World Applied Science Journal
Research Member
Research Rank
1
Research Vol
Vol. 12, No.4
Research Year
2011
Research Pages
PP. 519-530