3. Terminal velocity of an object in freefall is given by Vt = root 2gMA/Cdñ

,
where g is gravitational acceleration,Cd is the coefficient of drag, p is air density, and MA is the ratio M/A of mass M to ‘downwards facing’ area A. For a falling sphere of radius r, we calculate that dMA dr = 4/ 3 . Find an expression for dVt /dr .

Vt= sqrt (2mg/CpA}

d(m/A)/dr given =4/3

dVt/dr=1/2 * 1/Vt *g/Cp *d(m/A)/dr
= 1/2Vt*g*4/3Cp
= 2g/(3(Cp)Vt)

if I understand your problem statement correctly.

LOL - she sure has tough ones. It took me a while to figure out the landing on an optimal radius plant one.

m = mass = rho * (4/3) pi r^3

A =cross section area = pi r^2

m/A = rho * (4/3) r
d/dr (m/A) = (4/3) rho
NOTE DISAGREE

I guess the density of your sphere is one?

Vt is when
m g = C * p (1/2)Vt^2 A

Vt^2 = 2 m g /(pCA)

Vt = [2 m g /(pCA)]^.5
let MA = m/A
then
Vt = [2 g/pC]^.5 [ m/A]^.5

dVt/dr =[2 g/pC]^.5 *.5 [m/A]^-.5 d/dr [m/A]
but we know
d/dr [m/A] = rho [4/3]
so
dVt/dr =[2 g/pC]^.5 *.5 [m/A]^-.5 (4/3) rho
so
(2/3)rho [2 g/pC]^.5/(rho*(4/3)r)^.5

That can be simplified

To find an expression for dVt/dr, we need to differentiate the equation Vt = √(2gMA/Cdρ) with respect to r.

First, let's rewrite the equation to make it easier to differentiate:

Vt = √[(2gMA)/(Cdρ)]

Now, differentiate both sides of the equation with respect to r:

dVt/dr = 1/2 * (2gMA)/(Cdρ)^(-1/2) * d/dr(2gMA/Cdρ)

To simplify the expression, we need to find the derivative of 2gMA/Cdρ with respect to r.

Using the product and quotient rules of differentiation, we can break down the expression:

d/dr(2gMA/Cdρ) = (2g * dMA/dr * A * Cdρ - 2gMA * d(Cdρ)/dr) / (Cdρ)^2

Then, we substitute this expression back into our previous equation:

dVt/dr = 1/2 * (2gMA)/(Cdρ)^(-1/2) * [(2g * dMA/dr * A * Cdρ - 2gMA * d(Cdρ)/dr) / (Cdρ)^2]

Next, simplify the expression:

dVt/dr = gMA/(Cdρ) * [(dMA/dr * A * Cdρ - MA * d(Cdρ)/dr) / (Cdρ)]

Finally, if we substitute the given value of dMA/dr (dMA/dr = 4/3), we get:

dVt/dr = gMA/(Cdρ) * [(4/3 * A * Cdρ - MA * d(Cdρ)/dr) / (Cdρ)]