The expression for the orbital period is T = [tex]4\pi R^{\frac{3}{2} } / \sqrt{G(4M+m)}[/tex]
The force acting on one of the masses m by the other two is:
[tex]\frac{GMm}{R^{2} } + \frac{Gmm}{4R^{2} }[/tex]
This acts as the centripetal force and hence = mRω^2
So, [tex]\frac{GMm}{R^{2} } + \frac{Gmm}{4R^{2} }[/tex] = mRω^2
Solving this, we get ω = [tex]\sqrt{\frac{G(4M+m)}{4R^{3} } }[/tex]
We know that time period T = 2[tex]\pi[/tex]/ω
So , T = [tex]4\pi R^{\frac{3}{2} } / \sqrt{G(4M+m)}[/tex]
i.e. The expression for the orbital period is T = [tex]4\pi R^{\frac{3}{2} } / \sqrt{G(4M+m)}[/tex]
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