<DOC>
<DOCNO>
920
</DOCNO>
<TITLE>
supersonic flow over an inclined wing of zero aspect ratio .
</TITLE>
<AUTHOR>
stewartson, k.
</AUTHOR>
<BIBLIO>
proc. camb. phil. soc. v. 46, pt. 2, p307, april 1950 .
</BIBLIO>
<TEXT>
an asymptotic expression is found for the lift distribution on a long,
narrow, laminar wing, at incidence in a supersonic stream . the approximations
of the linearized potential theory are used .
</TEXT>
</DOC>
