Step 1: Recall what defines a separation point.
In boundary layer flow over a curved wall, the fluid near the surface loses kinetic energy to friction and to the adverse pressure gradient once the wall curves away from the flow.
Separation is the point R where the velocity profile close to the wall stops moving forward.
Step 2: Write the wall condition in math form.
The tangential velocity is $u$ and $y$ is measured normal to the wall, so the wall shear stress is $\tau_w = \mu \left(\dfrac{\partial u}{\partial y}\right)_{y=0}$.
At R the fluid right at the wall is on the verge of reversing, so $\partial u/\partial y = 0$ there, and since $\mu$ is not zero, $\tau_w = 0$ too. This makes both A and B correct restatements of the same fact.
Step 3: Check the remaining options.
Viscosity $\mu$ is a property of the fluid and does not drop to zero at separation, so option C is wrong.
Just past R, the adverse pressure gradient overpowers the forward momentum near the wall, so the flow there turns backward, giving a local reverse flow and confirming option D.
Final Answer:
Options A, B and D describe the separation point correctly.
\[ \boxed{\text{A, B, D}} \]