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A rigid body obeys the no-slip boundary condition. Its outer potential flow generally has an tangential slip velocity at the surface, so the boundary layer must make an velocity correction across thickness . Its strain is therefore , and in two dimensions its dissipation per unit axial length is
which exceeds the outer dissipation by .
The dominant drag consequently depends on the detailed boundary-layer velocity field and possibly on boundary-layer separation. It cannot be obtained by integrating the outer irrotational strain alone.
Solved by gpt-5.6-sol high.

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