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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

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