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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CP<br />
(C) <strong>of</strong>5 =<br />
o rrom Flg.ZJ<strong>of</strong> R<br />
19.90<br />
0.1<br />
0.2<br />
IT<br />
0.3<br />
04<br />
:-<br />
0.6<br />
. 20<br />
7,/I’ Calorically imparfect gas: T,=S00°R,T,,~380001<br />
Shock axpansion mathod<br />
---- Slandar oar<strong>of</strong>oil mathod y = yav<br />
I daal gas<br />
- - - - Shock axpansion mathod y ‘yInit ial<br />
0.3 0.4 0.5 ii 0.6 0.7 0.8 0.9<br />
Prossora distribution on lowar surfaca <strong>of</strong> IO% thick biconvax aar<strong>of</strong>oil saction at<br />
various anglas <strong>of</strong> attack-showing raal gas affacts (M = IO. To3 = 500’R)