How Do You Calculate Terminal Velocity for a Wooden Sphere Falling Through Air?

AI Thread Summary
To calculate the terminal velocity of a wooden sphere with a density of 0.870 g/cm³, radius of 8.00 cm, and drag coefficient of 0.500, the formula Vt = sqrt((2mg)/(C_D * ρ * A)) is used. The mass is calculated to be approximately 1.86585 kg, and the cross-sectional area is about 0.020106 m². Despite following the correct equations, the calculated terminal velocity of 55.1 m/s is disputed, suggesting potential issues with unit conversions or density values. The discussion highlights the importance of using consistent units and verifying the density of air, which can affect results. Overall, the calculations and methodology appear sound, but discrepancies in expected answers remain unresolved.
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Homework Statement



(a) Estimate the terminal speed of a wooden sphere (density 0.870 g/cm3) falling through air, if its radius is 8.00 cm and its drag coefficient is 0.500. (The density of air is 1.20 kg/m3.)
(b) From what height would a freely falling object reach this speed in the absence of air resistance?

Homework Equations



Vt = sqrt((2mg)/(DroeA))
v^2=2gx

The Attempt at a Solution



(A)
r=.08m
A=r^2pi=.020106
d=870kg/m^3
m=4/3pir^3*d=1.86585
so Vt should be sqrt((2(1.86585)g)/((.5)(1.2)(.020106))) or55.1
but it says that's wrong

can't start b without an a answer.
 
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Using those figures, I get the same answer.

I'm assuming you are using an online homework system? Does it specify what units it wants? Much of the problem is defined in terms of https://secure.wikimedia.org/wikipedia/en/wiki/CGS" . Perhaps try converting your answer to cm/s?
 
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nope, for sure mks... :( i was almost hoping i was doing something wrong.
 
anyone else have an idea?
 
is it possible that I'm using the wrong equation?
 
Probably not. I'm assuming this is an introductory physics course, so you're probably not being asked to model fluid flow with Navier-Stokes.

The dynamics of the system are, calling the drag force F and down positive:
m\mathbf{\ddot{x}} = m\mathbf{g} + \mathbf{F}.

Then, F is defined as:
\mathbf{F} = -C_D\frac{1}{2}\rho V^2 S \hat{\mathbf{V}} (i.e. opposite of velocity)

Since m\mathbf{\ddot{x}}=0 for terminal velocity, this leads to
0 = mg - C_D\frac{1}{2}\rho V^2 S

Solving for Vt:
V_t = \sqrt{\frac{2mg}{C_D\rho S}}

where CD is coefficient of drag, and S is cross-sectional area orthogonal to the flow.

So, that eqn. should work.
 
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