Concept:
Since in question not any velocity profile is given so we will use Blasius equation.
Calculation:
Pr = 1, T = 500 K, L = 1.5 m, T∞ = 300 K
\({\left( {{P_r}} \right)^{\frac{1}{3}}} = \frac{{{\delta _{hy}}}}{{{\delta _{th}}}} \Rightarrow \frac{{{\delta _{hy}}}}{{{\delta _{th}}}} = 1\)
∴ δhy = δth
\(Re = \frac{{\rho VD}}{\mu } = \frac{{VD}}{v} = \frac{{10 \times 0.5}}{{30 \times {{10}^{ - 6}}}} = 1.66 \times {10^5}\)
∵ Re ≤ 5 × 105
∴ Flow is laminar flow
∴ Blasius equation for laminar flow
\({\delta _{hy}} = \frac{{5x}}{{\sqrt {{R_{ex}}} }} = \frac{{5 \times 0.5}}{{\sqrt {1.66 \times {{10}^5}} }} \times 1000\;mm\)
δhy = 6.12 mm
δhy = δth = 6.12 mm
Mistake Point: While calculating Reynold number. Calculate the Reynold no. at a point at which hydrodynamic boundary length is required.