11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
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<strong>Supersonic</strong> parachute behavior<br />
Tests suggest that the performance of a parachute in<br />
transonic and supersonic flow is strongly influenced<br />
by:<br />
canopy porosity<br />
the size of the forebody (for axisymmetric bodies<br />
forebody diameter DB) D ) compared to the diameter of<br />
the parachute D0 represented by the ratio DB D / D0 D<br />
the distance between the base of the forebody and the<br />
parachute skirt (xT) ( ) represented by the ratio xT / DB; D<br />
the shape of the forebody (streamlined or bluff);<br />
line length;<br />
detail canopy design;<br />
Mach number