A Survey of Unsteady Hypersonic Flow Problems
A Survey of Unsteady Hypersonic Flow Problems
A Survey of Unsteady Hypersonic Flow Problems
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-0.02<br />
0<br />
’ 0.02<br />
cP<br />
0.04<br />
0.06<br />
O-08<br />
0.10<br />
/’<br />
I<br />
6<br />
0.12 L<br />
0<br />
0-I 0.2 0.3<br />
----- Unmodified Newtonian impact theory<br />
-- Modified Nuwtonian impact theory<br />
-.-- 3rd order piston theory<br />
Method <strong>of</strong> charactistics (Ref. 28)<br />
Pressure distribution on a loo/o thick biconvex aer<strong>of</strong>oil section (M = IO, as = 0”)