Consider the two-dimensional laminar boundary layer flow of air over a wide 15 cm long flat...

Consider the two-dimensional laminar boundary layer flow of air over a wide 15 cm long flat plate whose surface temperature varies linearly from 20°C at the leading edge to 40°C at the trailing edge. This plate is placed in an airstream with a velocity of 2 m/s and a temperature of 10°C. Numerically determine how the surface heat flux varies along the plate.
Explain the results obtained with proper reasoning. Support your results with scaling analysis wherever possible.I need c++ program to solve the similarity equations.

Expert Solution

samet mamat answered 1 year ago

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