Tanya Sharma said:
Sorry...I still do not understand why this relation holds .I understand the angle you are talking about but why the tangent of that angle is equal to the ratio of tangential and radial components of velocity.
I have attached one more picture, I wonder if it is going to help.
You can do it another way too. Assume that the first mass is at ##\vec{r_1}##, the second one at ##\vec{r_2}## and the third one at ##\vec{r_3}##. You can write these three vectors in the following way:
$$\vec{r_1}=r\cos\theta \hat{i}+r\sin\theta \hat{j}$$
$$\vec{r_2}=r\cos\left(\theta+\frac{2\pi}{3}\right)\hat{i}+r\sin\left( \theta+\frac{2\pi}{3}\right)\hat{j}$$
$$\vec{r_3}=r\cos\left(\theta+\frac{4\pi}{3}\right)\hat{i}+r\sin\left( \theta+\frac{4\pi}{3}\right)\hat{j}$$
Do you see that the following relation holds?
$$\left(\vec{r_2}-\vec{r_1}\right)\times \frac{d\vec{r_1}}{dt}=0$$
If so, can you use the above to find some useful info?
Remember, we are working in a coordinate system where the centroid of the triangle formed by the initial position of masses is at origin.
I think that gives a DE in r and θ ? How do you get DE in r and t ?
From the relation above, you get
$$r\dot{\theta}=-\frac{\dot{r}}{\sqrt{3}}$$
Plug this in
$$u^2=\dot{r}^2+(r\dot{\theta})^2 \Rightarrow 3u^2=4\dot{r}^2$$