Correct Answer - `(1-y/h)`
Case I:
Drag force `F_(1) +F_(2)`
`[eta_(0)v/(h//2)+eta_(0)v/(h//2)]A`
Case II:
Drag force on the plane
`=[eta-v/(h-y)+etav/y]A=(etavha)/(y(h-y))`
In both cases drag force are equal
`implies(4eta_(0)vA)/h=(etavha)/(y(h-a))`
`implies eta=(4eta_(0))/h(1-y/h)`
