32nd Aerospace Sciences Meeting & Exhibit: 94-0640 - 94-0669American Institute of Aeronautics and Astronautics, 1994 - Aeronautics |
Common terms and phrases
3-D TBL Aerospace Sciences Meeting AIAA AIAA Paper Aircraft airfoil algorithm angle angle of attack average axisymmetric Blasius Solution 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 downstream duct dynamic dynamic modulus effect equations exit experimental flat plate flow field Fluid Mechanics flux freestream frequency grid Hypersonic images incoming boundary layer interaction laminar laser linear LU-ADI Mach number measured mesh method modulus Navier-Stokes Navier-Stokes equations nozzle obtained parameters particle plane present reconstruction region Reynolds number Scalar scheme shear layer shock shown in Figure simulation solver spanwise spatial streamwise 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 wall wind tunnel Yaw Angle