For a straight pipe with cross-section , , steady unidirectional incompressible flow reduces the Navier-Stokes equations to , with constant axial pressure gradient. The displayed cubic polynomial vanishes on every wall, and its transverse Laplacian is . The axial drag per unit length on each of the three equal walls is . This follows by integrating the viscous traction on one wall; summing the three forces equals the pressure gradient times the triangular area.
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