<DOC>
<DOCNO>
1276
</DOCNO>
<TITLE>
a three-dimensional linearized analysis of the forces
exerted on a rigid wing by a shock wave .
</TITLE>
<AUTHOR>
ehlers,f.e. and shoemaker,e.m.
</AUTHOR>
<BIBLIO>
j. ae. scs. 1960, 257.
</BIBLIO>
<TEXT>
  the pressure distribution on a moving flat plate induced by an
acoustic shock front striking the edge of the plate obliquely has
been found in terms of the two-dimensional solution of the authors
</TEXT>
</DOC>
