If you could, please plot im sheets After it is solved. A jet aircraft have the following parameters:

$C_{D0}=0\mathrm{.}0216,S=230f{t}^2,b=34ft,W=13000lbf,e=0\mathrm{.}82,V=400knts$

$=0\mathrm{.}0023769$ slug $\frac{?}{f{t}^3}$

Determine a$.$ minimum thrust required in pounds force, b$.$ velocity for minim thrust required in

knots, c$.$ lift coefficient for minim thrust required, and drag coefficient for minimum thrust

required. In addition, plot thrust or drag vs$.$ airspeed and the available thrust is $10000$ lbf $.$

For the aircraft in Problem $1,$

Determine a$.$ minimum power required in horsepower, b$.$ velocity for minimum power required

in knots, c$.$ lift coefficient for minimum power required, and drag coefficient for minimum

power required.