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 />
o-02<br />
CP<br />
0.04<br />
0.06<br />
0.00<br />
0.10<br />
0*12<br />
4<br />
f<br />
/’<br />
4 . / -.--<br />
/:<br />
/<br />
Slender aer<strong>of</strong>oil method<br />
-- - - Shock expansion method<br />
Method <strong>of</strong> charactaristics<br />
0.2 o-3 0.4 0.5 2 O-6 0.7 0.8 0.9 I<br />
Pressure distribution on loo/o thick biconvex aar<strong>of</strong>oil section (M = IO, as = 0’)