<DOC>
<DOCNO>
382
</DOCNO>
<TITLE>
a note on the laminar boundary layer on a circular cylinder in
axial incompressible flow .
</TITLE>
<AUTHOR>
howard r. kelly
</AUTHOR>
<BIBLIO>
u.s. naval ordnance test station, inyokern, china lake, calif.
</BIBLIO>
<TEXT>
a correction is made for the equation to compute the ratio
of the displacement thickness on a cylinder to the corresponding
thickness on a flat plate .
</TEXT>
</DOC>
