Step 1: Understanding boundary layer thickness.
For a laminar boundary layer over a flat plate, the thickness of the boundary layer \( \delta \) at a distance \( x \) from the leading edge is given by the formula:
\[
\delta \sim x^{\frac{1}{2}}
\]
This formula is derived from the solution of the Navier-Stokes equations for laminar flow over a flat plate.
Step 2: Conclusion.
The boundary layer thickness varies as \( x^{\frac{1}{2}} \) for laminar flow.
Final Answer:
\[
\boxed{x^{\frac{1}{2}}}
\]