Numerical Solution of the Navier-Stokes Equations for a Shock-boundary Layer Interaction Problem Using an L-U Implicit Scheme |
Contents
II | 14 |
Coordinate Transformation | 22 |
Notation for Discretization | 26 |
6 other sections not shown
Common terms and phrases
55 SECOND GRID approximately B₂ boundary conditions boundary layer BOUNDARY LAYER THEORY BURATYNSKI LU IMPLICIT Buratynski's LU scheme cartesian grid central differences Convergence Histories Courant number eigenvalues EMPLOYING BURATYNSKI LU equa EULER EQUATIONS evaluated explicit boundary conditions fictitious points finite volume method first-order-accurate flow Flux Vector Splitting free-stream implicit operator implicit portion interac INTERACTION MACH 2.00 inviscid shock reflection LAYER INTERACTION MACH layer interaction problem leading edge left hand side LU factoring LU IMPLICIT SCHEME MACH 2.00 SIGMA Mach number matrix MESH SIZE NX mesh spacing Navier-Stokes equations no-slip conditions non-dimensional number of space numerical smoothing terms numerical solution optimum parameters physical domain plate surface PRESSURE CONTOUR Reynolds number SECOND GRID SYSTEM shock waves SHOCK-BOUNDARY LAYER INTERACTION shown in Figure skin friction solving the Navier-Stokes Splitting Implicit scheme sweep time-level tion variables Vector Splitting Implicit vergence x-velocity Profiles y-direction อพ