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3-D TBL accuracy AIAA AIAA Paper Aircraft airfoil algorithm angle angle of attack average axisymmetric boundary layer boundary layer thickness bow shock calculated cell centered expansion centerline coefficient compressible configuration contours convective convergence curvature cylinder delta wing developed diameter dimensional distribution domain downstream duct dynamic dynamic modulus effect exit experimental flat plate flow field Fluid Mechanics flux Formulation freestream frequency grid images implicit incoming boundary layer interaction laminar laser linear Mach number measured mesh method modulus Navier-Stokes equations nozzle obtained parameters particle plane present problem reconstruction region Reynolds number Scalar scheme shear layer shock shown in Figure simulation solution solver spanwise spatial streak streamwise stress structures subsonic supersonic surface temperature tions turbulence model turbulent boundary layer turbulent flow unstructured unstructured grid unstructured-grid upwind USLIP values velocity Velocity Profile computed viscoelastic viscous vortex vorticity wake wall wind tunnel Yaw Angle