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Question

A spherical body of radius $r$ and density $\sigma$ falls freely through a viscous liquid having density $\rho$ and viscosity $\eta$ and attains a terminal velocity $v_0$. Estimated maximum error in the quantity $\eta$ is : (Ignore errors associated with $\sigma, \rho$ and $g$, gravitational acceleration)

The correct answer is
$2 \frac{\Delta r}{r} - \frac{\Delta v_0}{v_0}$

Derivation of Viscosity Formula

Terminal velocity ($v_0$) is achieved when the net force on the sphere is zero. The forces involved are gravitational ($F_g$), buoyancy ($F_b$), and viscous drag ($F_d$).

  • $F_g = \frac{4}{3}\pi r^3 \sigma g$
  • $F_b = \frac{4}{3}\pi r^3 \rho g$
  • $F_d = 6\pi \eta r v_0$

Setting $F_g - F_b = F_d$ gives:

$ \frac{4}{3}\pi r^3 (\sigma - \rho)g = 6\pi \eta r v_0 $

Solving for the viscosity ($\eta$):

$ \eta = \frac{4 \pi r^3 (\sigma - \rho)g}{3 \times 6 \pi r v_0} = \frac{2 r^2 (\sigma - \rho)g}{9 v_0} $

Error Propagation Analysis

We analyze the error in $\eta$ considering its dependence on radius $r$ and terminal velocity $v_0$. The other terms ($\sigma$, $\rho$, $g$) are assumed to have negligible errors.

Let $\eta$ be represented as:

$ \eta(r, v_0) = K \frac{r^2}{v_0} $

where $K = \frac{2 (\sigma - \rho)g}{9}$ is treated as a constant.

The change in $\eta$, denoted $\Delta \eta$, can be approximated using partial derivatives:

$ \Delta \eta \approx \frac{\partial \eta}{\partial r} \Delta r + \frac{\partial \eta}{\partial v_0} \Delta v_0 $

Calculate the partial derivatives:

  • $ \frac{\partial \eta}{\partial r} = \frac{\partial}{\partial r} \left( K \frac{r^2}{v_0} \right) = K \frac{2r}{v_0} $
  • $ \frac{\partial \eta}{\partial v_0} = \frac{\partial}{\partial v_0} \left( K \frac{r^2}{v_0} \right) = - K \frac{r^2}{v_0^2} $

Substitute these into the error approximation:

$ \Delta \eta \approx \left( K \frac{2r}{v_0} \right) \Delta r + \left( - K \frac{r^2}{v_0^2} \right) \Delta v_0 $ $ \Delta \eta \approx K \frac{2r \Delta r}{v_0} - K \frac{r^2 \Delta v_0}{v_0^2} $

Calculating Relative Error

The question asks for the error in $\eta$. The options provided are in terms of relative errors. We calculate the relative error $\frac{\Delta \eta}{\eta}$:

$ \frac{\Delta \eta}{\eta} \approx \frac{K \frac{2r \Delta r}{v_0} - K \frac{r^2 \Delta v_0}{v_0^2}}{K \frac{r^2}{v_0}} $

Simplifying the expression:

$ \frac{\Delta \eta}{\eta} \approx \frac{K \frac{2r \Delta r}{v_0}}{K \frac{r^2}{v_0}} - \frac{K \frac{r^2 \Delta v_0}{v_0^2}}{K \frac{r^2}{v_0}} $ $ \frac{\Delta \eta}{\eta} \approx 2 \frac{\Delta r}{r} - \frac{\Delta v_0}{v_0} $

This result matches the expression in Option D.

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