Carefully selected blend of computational techniques solves complete set of equations for viscous, unsteady, hypersonic flow in general curvilinear coordinates. New algorithm has tested computation of axially directed flow about blunt body having shape similar to that of such practical bodies as wide-body aircraft or artillery shells. Method offers significant computational advantages because of conservation-law form of equations and because it reduces amount of metric data required.
Numerical Solution for Navier-Stokes Equations
NASA Tech Briefs ; 6 , 3
1982-12-01
Sonstige
Keine Angabe
Englisch
Numerical Solution Of Navier-Stokes Equations
NTRS | 1989
|Numerical integration of Navier-Stokes equations
AIAA | 1970
|