<DOC>
<DOCNO>
264
</DOCNO>
<TITLE>
asymptotic solution of the two dimensional oscillating
aerofoil problem for high subsonic mach numbers .
</TITLE>
<AUTHOR>
eckhaus,w.
</AUTHOR>
<BIBLIO>
proc. 9th int. con. app.mech. 1956.
</BIBLIO>
<TEXT>
  a new method has been given, for obtaining asymptotic solutions of a
boundary value problem for the wave equation .  the method is simpler
than the method previously given by burger, and leads to a result
identical with burger's result .
</TEXT>
</DOC>
