<DOC>
<DOCNO>
326
</DOCNO>
<TITLE>
forst-order slip effects on the compressible laminar
boundary layer over a slender body of revolution in
axial flow .
</TITLE>
<AUTHOR>
shen,s.f. and solomon,j.m.
</AUTHOR>
<BIBLIO>
j.ae.scs. 28, 1961.
</BIBLIO>
<TEXT>
analysis of the
compressible boundary layer with transverse curvature in first order
slip flow .  no boundary-layer interaction effects are considered
and only the zero pressure-gradient case is examined .
</TEXT>
</DOC>
