11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
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CP<br />
Drag of bluff body<br />
2.50<br />
2.00<br />
1.50<br />
1.00<br />
0.50<br />
0.00<br />
-0.50<br />
0 0.5 1 1.5 2 2.5<br />
Mach number<br />
1.2<br />
1<br />
0.8<br />
0.6<br />
0.4<br />
0.2<br />
0<br />
Cp stagnation<br />
Cp base<br />
Cp total<br />
CD
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