Computation of boundary layer flow using thinlayer NavierStokes equations with fluxvector splitting
Abstract
The thinlayer compressible NavierStokes equations are used for the calculation of boundary layer flows. A fluxvector splitting technique is applied for the convective parts of the fluxes, the viscous parts are centrally differenced. The computed flow cases include flat plate boundary layer flows with free stream Mach numbers of 0.3 (nearly incompressible) and 4, and the flow of shock and boundary layer interaction with the free stream Mach number of 2. The calculations are compared with theoretical and experimental results.
 Publication:

NASA STI/Recon Technical Report N
 Pub Date:
 October 1989
 Bibcode:
 1989STIN...9110254P
 Keywords:

 Boundary Layer Flow;
 Boundary Layers;
 Computational Fluid Dynamics;
 Flux Vector Splitting;
 NavierStokes Equation;
 Shock Layers;
 Subsonic Speed;
 Boundary Conditions;
 Computational Grids;
 Convection;
 Flat Plates;
 Free Flow;
 Supersonic Speed;
 Fluid Mechanics and Heat Transfer