Engineering, 06.08.2021 16:10 carlossauceda0
A laminar boundary layer velocity profile is approximated by u / U = [ 2 − ( y / δ ) ] ( y / δ ) u/U=[2−(y/δ)](y/δ) for y ≤ δ y≤δ, and u = U u=U for y > δ y>δ.
(a) Show that this parabolic profile satisfies the appropriate boundary conditions.
(b) Use the momentum integral equation to determine the boundary layer thickness, δ = δ ( x ) δ=δ(x). Compare the result with the exact Blasius solution.
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A laminar boundary layer velocity profile is approximated by u / U = [ 2 − ( y / δ ) ] ( y / δ ) u/U...
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