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You contact the jumpers used to generate the data in the table below and measure their frontal areas.

m$,$ kg $83\mathrm{.}660\mathrm{.}272\mathrm{.}191\mathrm{.}192\mathrm{.}965\mathrm{.}380\mathrm{.}9$

vt$,$ m$/$s $53\mathrm{.}448\mathrm{.}550\mathrm{.}955\mathrm{.}75447\mathrm{.}751\mathrm{.}1$

The resulting values, which are ordered in the same sequence as the corresponding values in the table above, are

A$,$ m$20\mathrm{.}4550\mathrm{.}4020\mathrm{.}4520\mathrm{.}4860\mathrm{.}5310\mathrm{.}4750\mathrm{.}487$

If the air density is $\backslash$rho $=1\mathrm{.}422$ kg$/$m$3,$ use MATLAB to compute values of the dimensionless drag coefficient CD$.($Round the final answers to four decimal places.$)$

The values of the drag coefficient CD are listed as follows: