Add to ORKGThe Parabolized Navier-Stokes (PNS) equations form a subset of the Navier-Stokes equations . This report contains the details of the development of the PNS equations from the Navier-Stokes equations for an ideal gas model (7 - constant) . The resulting equations are numerically solved In a generalized coordinate system using a finite-difference implementation of MacCormack's explicit predictor-corrector algorithm . A three-dimensional code based on this algorithm has been developed and applied to the ideal gas flow past a right circular cone at 0 deg angle of attac
A numerical code has been developed to solve the Viscous Shock Layer (VSL) equations for chemically ...
A two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and n...
This report consists of two published papers, 'Computation of Magnetohydrodynamic Flows Using an Ite...
The Parabolized Navier-Stokes (PNS) equations form a subset of the Navier-Stokes equations . This re...
In this lecture we will (1) develop the governing PNS (Parobolized Navier-Stokes) equations for idea...
A stable , accurate amp; efficient implementation of MacCormack's algorithm for the inviscid limit o...
The hypersonic (M = 25) flow past a 100 right circular cone at 0 angle of attack has been computed u...
Under specific assumptions, parabolized Navier-Stokes equations are a suitable mean to study channel...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
A new parabolized Navier-Stokes (PNS) code has been developed to compute the hypersonic, viscous che...
Two new parabolized Navier-Stokes (PNS) codes were developed to compute the three-dimensional, visco...
Flows of relevance to new generation aerospace vehicles exist, which are weakly de-pendent on the st...
Two new parabolized Navier-Stokes (PNS) codes have been developed to compute the hypersonic flow of ...
Subject of inquiry: supersonic viscous impact layer. The aim of the work is to develop efficient num...
The flow of the compressible gas is investigated by means of the developed finite-difference compute...
A numerical code has been developed to solve the Viscous Shock Layer (VSL) equations for chemically ...
A two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and n...
This report consists of two published papers, 'Computation of Magnetohydrodynamic Flows Using an Ite...
The Parabolized Navier-Stokes (PNS) equations form a subset of the Navier-Stokes equations . This re...
In this lecture we will (1) develop the governing PNS (Parobolized Navier-Stokes) equations for idea...
A stable , accurate amp; efficient implementation of MacCormack's algorithm for the inviscid limit o...
The hypersonic (M = 25) flow past a 100 right circular cone at 0 angle of attack has been computed u...
Under specific assumptions, parabolized Navier-Stokes equations are a suitable mean to study channel...
A new computer code for the solution of the three-dimensional parabolized Navier-Stokes (PNS) equati...
A new parabolized Navier-Stokes (PNS) code has been developed to compute the hypersonic, viscous che...
Two new parabolized Navier-Stokes (PNS) codes were developed to compute the three-dimensional, visco...
Flows of relevance to new generation aerospace vehicles exist, which are weakly de-pendent on the st...
Two new parabolized Navier-Stokes (PNS) codes have been developed to compute the hypersonic flow of ...
Subject of inquiry: supersonic viscous impact layer. The aim of the work is to develop efficient num...
The flow of the compressible gas is investigated by means of the developed finite-difference compute...
A numerical code has been developed to solve the Viscous Shock Layer (VSL) equations for chemically ...
A two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and n...
This report consists of two published papers, 'Computation of Magnetohydrodynamic Flows Using an Ite...