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

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Mechanical Engineering

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

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