<DOC>
<DOCNO>
250
</DOCNO>
<TITLE>
pressure distributions at zero lift for delta wings
with rhombic cross sections .
</TITLE>
<AUTHOR>
eminton,e.
</AUTHOR>
<BIBLIO>
arc cp.525, 1960.
</BIBLIO>
<TEXT>
  the linearised theory of thin wings is used to calculate pressure
distributions over delta wings with rhombic cross sections .  a deuce
programme has been written for the calculation and some of the results
are compared with those of slender thin wing theory .
</TEXT>
</DOC>
