Using MATLAB, code this please

Aircraft Turning Radius An object moving in a circular path at a constant

tangential velocity v is shown in Figure $2\mathrm{.}26.$ The radial acceleration

required for the object to move in the circular path is given by the

Equation $(2\mathrm{.}62)$:

a$=$v$^2/$r

where a is the centripetal acceleration of the object in m$/$s$2,$ v is the tangential

velocity of the object in m$/$s$,$ and r is the turning radius in meters.

Suppose that the object is an aircraft, and answer the following questions

about it$.$

$($a$)$ Suppose that the aircraft is moving at Mach $0\mathrm{.}85,$ or $85$ percent

of the speed of sound. If the centripetal acceleration is $2$ g$,$ what

is the turning radius of the aircraft? $($Note: For this problem,

you may assume that Mach $1$ is equal to $340$ m$/$s and that $1$ g

$9\mathrm{.}81$ m$/$s$2.)$

$($b$)$ Suppose that the speed of the aircraft increases to Mach $1\mathrm{.}5.$ What is

the turning radius of the aircraft now?

$($c$)$ Plot the turning radius as a function of aircraft speed for speeds

between Mach $0\mathrm{.}5$ and Mach $2\mathrm{.}0,$ assuming that the acceleration

remains $2$ g$.$

$($d$)$ Suppose that the maximum acceleration that the pilot can stand is

$7$ g$.$ What is the minimum possible turning radius of the aircraft at

Mach $1\mathrm{.}5?$

$($e$)$ Plot the turning radius as a function of centripetal acceleration for

accelerations between $2$ g and $8$ g$,$ assuming a constant speed of

Mach $0\mathrm{.}85.$