11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
11 - Supersonic parachutes Lingard.pdf
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Aerodynamic Heating<br />
stagnation temperature<br />
TT SS =<br />
= TT 00 [<strong>11</strong> + rr{ { ( γγ -- <strong>11</strong> ) / 22}<br />
convection<br />
Q Q = = h h ( TT SS -- TT WW )<br />
radiation<br />
QQ = - εε σσ TT 44<br />
WW<br />
} MM 22 ]