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JEE Advanced 2026 · System of Particles and Rotational Motion

A particle of mass mm, and angular momentum ℓ\ell is moving in a circular orbit of radius r0r_0 under the influence of an attractive force F⃗(r)=−kr2r^\vec{F}(r) = -\frac{k}{r^2}\hat{r}. Keeping its angular momentum unchanged, the particle is displaced radially by a small distance δr≪r0\delta r \ll r_0, due to which its radial distance varies periodically. The corresponding time period is:

Answer: A. 2πℓ3mk2\frac{2\pi\ell^{3}}{mk^{2}}

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Written solution

Step 1: Analyze the initial circular orbit.

For a circular orbit of radius r0r_0, the centripetal force is provided by the attractive central force.

mv2r0=kr02\frac{m v^2}{r_0} = \frac{k}{r_0^2}

The angular momentum ℓ\ell is given by:

ℓ=mvr0\ell = m v r_0

Step 2: Relate the angular momentum to the orbit radius.

Eliminating the velocity vv from the circular orbit equations yields the relationship between ℓ\ell and r0r_0.

ℓ2=mkr0\ell^2 = m k r_0 r0=ℓ2mkr_0 = \frac{\ell^2}{mk}

Step 3: Define the effective potential.

The radial motion of the particle is described using the one-dimensional effective potential Ueff(r)U_{\text{eff}}(r).

Ueff(r)=ℓ22mr2−krU_{\text{eff}}(r) = \frac{\ell^2}{2mr^2} - \frac{k}{r}

Step 4: Find the first derivative of the effective potential.

The equilibrium radius r0r_0 corresponds to the minimum of the effective potential.

dUeffdr=−ℓ2mr3+kr2\frac{dU_{\text{eff}}}{dr} = -\frac{\ell^2}{mr^3} + \frac{k}{r^2}

Setting this derivative to zero at r=r0r = r_0 confirms the circular orbit condition.

−ℓ2mr03+kr02=0-\frac{\ell^2}{mr_0^3} + \frac{k}{r_0^2} = 0 ℓ2=mkr0\ell^2 = m k r_0

Step 5: Set up the equation of motion for small radial oscillations.

For a small radial displacement r=r0+δrr = r_0 + \delta r where δr≪r0\delta r \ll r_0, the equation of motion is obtained by Taylor expanding about the minimum.

mδr¨=−Ueff′′(r0)δrm \delta\ddot{r} = -U_{\text{eff}}''(r_0) \delta r

Step 6: Calculate the second derivative of the effective potential.

Differentiate the first derivative with respect to rr.

Ueff′′(r)=3ℓ2mr4−2kr3U_{\text{eff}}''(r) = \frac{3\ell^2}{mr^4} - \frac{2k}{r^3}

Evaluate this second derivative at r=r0r = r_0 using the relation ℓ2=mkr0\ell^2 = m k r_0.

Ueff′′(r0)=3kr03−2kr03U_{\text{eff}}''(r_0) = \frac{3k}{r_0^3} - \frac{2k}{r_0^3} Ueff′′(r0)=kr03U_{\text{eff}}''(r_0) = \frac{k}{r_0^3}

Step 7: Determine the angular frequency of the radial oscillations.

The angular frequency ωr\omega_r is determined by the effective spring constant.

ωr2=Ueff′′(r0)m\omega_{r}^2 = \frac{U_{\text{eff}}''(r_0)}{m} ωr2=kmr03\omega_{r}^2 = \frac{k}{mr_0^3}

Step 8: Express the angular frequency in terms of angular momentum.

Substitute r0=ℓ2mkr_0 = \frac{\ell^2}{mk} into the expression for ωr2\omega_r^2.

ωr2=km(mkℓ2)3\omega_{r}^2 = \frac{k}{m} \left(\frac{mk}{\ell^2}\right)^3 ωr2=m2k4ℓ6\omega_{r}^2 = \frac{m^2 k^4}{\ell^6} ωr=mk2ℓ3\omega_{r} = \frac{mk^2}{\ell^3}

Step 9: Calculate the time period of the radial oscillations.

The time period TT is related to the angular frequency by T=2πωrT = \frac{2\pi}{\omega_r}.

T=2πℓ3mk2T = \frac{2\pi\ell^3}{mk^2}

Answer: The corresponding time period is T=2πℓ3mk2T = \dfrac{2\pi\ell^3}{mk^2}.

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