3-Dimensional Boundary Layer Generated by a Spinning Body
Sample Data Plots
The plots below show the wall skin friction coefficients \(C_{fx}\) and \(C_{fz}\) for three spin ratios in the C cases.
The plot below shows the pressure coefficient distribution for various adverse pressure gradient cases.
The plots below show profiles of the normalized mean velocities and Reynolds stresses at a selection of streamwise locations for the A.S1 case (zero pressure gradient, with spin ratio of 1).