11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
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<strong>Supersonic</strong> flow around <strong>parachutes</strong><br />
Dominated by interaction with viscous wake<br />
At low supersonic Mach number conical shock<br />
forms and reduces drag<br />
At higher Mach number forebody base flow is<br />
disrupted cyclically and parachute pulsation<br />
commences with large drag loss