In the laminar flow of air ($P_r$ = $0.7$) over a heated plate, if $\delta$ and $\delta _T$ denote, respectively, the hydrodynamic and thermal boundary layer thicknesses, then
- $\delta =\delta _T$
- $\delta > \delta _T$
- $\delta < \delta _T$
- $\delta =0$ but $\delta _T\neq 0$