IX. Boundary layer Profile Properties
To the practicing engineer the velocity profile itself is of very little interest. The following parameters are more important.
1. Boundary Layer Thickness d: This is defined as the y- location where u/ue reaches 0.99%, that is the u- velocity becomes 99% of the edge velocity.
2. Displacement Thickness d* : This is a measure of the outward displacement of the streamlines from the solid surface as a result of the reduced u- velocity within the boundary layer. This quantity is defined as
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where the subscript 'e' refers to the conditions at the boundary layer edge. This quantity is usually computed by numerical integration.
3. Momentum Thickness
q: This is a measure of the momentum loss within the boundary layer as a result of the reduced velocities within the boundary layer. It is defined as![]()
and may be found by numerical integration of the velocity profile.
4. Shape Factor H : This quantity is defined as the ratio
d*/q . For laminar flows H varies between 2 and 3. It is 3.7 near separation point. Thus excessively large values of H (above 3) indicate that the boundary layer is about to separate. In turbulent flows, H varies between 1.5 and 2.5. Surface Shear Stress: The shear stress at the wall can be found from the definition of shear stress (See Handout #1). It is given by,
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6. Skin friction Coefficient cf:The derivative of u is computed numerically. This quantity is usually non-dimensionalized by the dynamic pressure at the boundary layer edge, giving the skin friction coefficient cf as

7. Skin Friction Drag, D : The shear stress may be numerically integrated over the entire solid surface to give the skin friction drag force along the x- axis:
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8. Skin Friction Drag Coefficient Cd: The drag force is usually non-dimensionalized by the freestream dynamic pressure times the chord of the airfoil c, giving the skin friction drag coefficient along the x- axis, Cd.

Important: Note that all of the above definitions hold for laminar and turbulent, compressible and incompressible boundary layers!