A rapid implicit-explicit solution to the two-dimensional time dependent incompressible Navier-Stokes equations
Abstract
A second-order time-accurate and spatially factored algorithm was used in a finite difference scheme for the numerical solution of the time-dependent, incompressible, two dimensional Navier-Stokes equations in conservation-law form using vorticity and stream function variables. The systems of equations are solved at each time step by an iterative technique. Numerical results were obtained for a circular cylinder at a Reynolds number of 15, and an NACA 0012 airfoil at zero angle of attack at Reynolds numbers of 10 to the third and 10 to the fourth powers. The results are in agreement with another numerical technique, and the computing time required to obtain the steady state solution at the Reynolds number of 10 to the 4th power was 49.7 sec on CDC 7600 computer using a 65 x 84 computational grind.
- Publication:
-
National Aeronautics and Space Administration Report
- Pub Date:
- October 1980
- Bibcode:
- 1980nasa.reptS....D
- Keywords:
-
- Finite Difference Theory;
- Incompressible Flow;
- Laminar Flow;
- Navier-Stokes Equation;
- Time Dependence;
- Two Dimensional Flow;
- Airfoils;
- Cdc 7600 Computer;
- Circular Cylinders;
- Iterative Solution;
- Stream Functions (Fluids);
- Vortices;
- Fluid Mechanics and Heat Transfer