I Terminal Velocity proportional to the Drag Force 𝑚𝛾𝑣² in free fall

[Victor Correa]

Can anyone help me? I know that's wrong, but i don't know where.

Thanks for your attention so far.

 

[hutchphd]

What question do you wish to find out?

 

[PeterDonis]

@Victor Correa putting content in attachments is not acceptable. You need to post your content directly in the forum, using the PF LaTeX feature for equations. There is a LaTeX Guide link at the bottom left of the edit window when you are composing a post.

 

[vanhees71]

Obviously in #1 the OP looks for the solution of the equation of motion for free fall including air resistance,
$$\ddot{x}=\dot{v}=g-\gamma v^2.$$
This equation for $v$ can obviously solved by separation of variables,
$$\mathrm{d} t = \frac{\mathrm{d} v}{g-\gamma v^2}.$$
We need the integral
$$\int \mathrm{d} v \frac{1}{g-\gamma v^2} = \frac{1}{g} \int \mathrm{d} v \frac{1}{1-(\sqrt{\gamma/g}v)^2} = \frac{1}{\sqrt{g \gamma}} \text{artanh} \left (\sqrt{\frac{\gamma}{g}} v \right).$$
With the initial condition $v(0)=0$ we thus get
$$t=\frac{1}{\sqrt{g \gamma}} \text{artanh} \left (\sqrt{\frac{\gamma}{g}} v \right).$$
Solved for $v$ you get
$$v(t)=\sqrt{\frac{g}{\gamma}} \tanh (\sqrt{g \gamma} t).$$
The terminal velocity is
$$v_{\infty} = \sqrt{\frac{g}{\gamma}}.$$

 

[erobz]

Yeah,after the $u$ substitution things get messy in your solution.

Leave the LHS as:

$$ \frac{1}{\gamma} \int \frac{dv}{ \left(\sqrt{ \frac{g}{\gamma }}\right)^2 -v^2 }= \frac{1}{\gamma} \int \frac{A dv}{\sqrt{\frac{g}{\gamma}} + v}+\frac{1}{\gamma} \int \frac{B dv}{\sqrt{\frac{g}{\gamma}} -v}$$

and continue with the partial fraction decomposition from there.

 

[mjc123]

The error you make is saying that the integral of du/(1-u) = ln(1-u)

 

[Victor Correa]

What question do you wish to find out?

The terminal velocity equation as a function of the coefficient γ²

 

[Victor Correa]

@Victor Correa putting content in attachments is not acceptable. You need to post your content directly in the forum, using the PF LaTeX feature for equations. There is a LaTeX Guide link at the bottom left of the edit window when you are composing a post.

Oh, I didn't know. Sorry

 

[Victor Correa]

Obviously in #1 the OP looks for the solution of the equation of motion for free fall including air resistance,
$$\ddot{x}=\dot{v}=g-\gamma v^2.$$
This equation for $v$ can obviously solved by separation of variables,
$$\mathrm{d} t = \frac{\mathrm{d} v}{g-\gamma v^2}.$$
We need the integral
$$\int \mathrm{d} v \frac{1}{g-\gamma v^2} = \frac{1}{g} \int \mathrm{d} v \frac{1}{1-(\sqrt{\gamma/g}v)^2} = \frac{1}{\sqrt{g \gamma}} \text{artanh} \left (\sqrt{\frac{\gamma}{g}} v \right).$$
With the initial condition $v(0)=0$ we thus get
$$t=\frac{1}{\sqrt{g \gamma}} \text{artanh} \left (\sqrt{\frac{\gamma}{g}} v \right).$$
Solved for $v$ you get
$$v(t)=\sqrt{\frac{g}{\gamma}} \tanh (\sqrt{g \gamma} t).$$
The terminal velocity is
$$v_{\infty} = \sqrt{\frac{g}{\gamma}}.$$

You are my hero !

 

[hutchphd]

The terminal velocity equation as a function of the coefficient γ²

So that is easy indeed $$\ddot{x}=\dot{v}=g-\gamma v^2.$$ Just demand$$\dot{v}=g-\gamma v^2=0.$$

 

[Victor Correa]

So that is easy indeed $$\ddot{x}=\dot{v}=g-\gamma v^2.$$ Just demand$$\dot{v}=g-\gamma v^2=0.$$

My problem is this

 

[erobz]

My problem is this

Yeah, you had a bit of a "can't see the forest through the trees" issue.