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Flow Over Flat Plate Comparison of ANSYS, FLUENT and
Theoretical Solution Tyre Bateman Kevin Price William Blattman
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Problem Statement 20 °C v = 0.5 m/s 0.25 m Tsurface = 50 °C 1 m
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Governing Equations/Known Values
Theoretical δ = 5.0/(u∞/νx) yt = δ ·Pr3 Analytical (u/ u∞) = 0.99 [(Ts-T)/(Ts-T∞)] = 0.99 u∞ = 0.5 m/s ν = e-05 Pr = 0.713 Tsurface = 50 °C Tair = 20 °C
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ANSYS Velocity/Temp Velocity boundary layer Temperature boundary layer
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Fluent Velocity/Temp Velocity boundary layer
Temperature boundary layer
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Theoretical vs. Analytical Velocity Boundary Layer
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Theoretical vs. Analytical Temperature Boundary Layer
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