An overview of parabolic and PNS (Parabolized Navier-Stokes) methodology developed to treat highly curved sub and supersonic wall jets is presented. The fundamental data base to which these models were applied is discussed in detail. The analysis of strong curvature effects was found to require a semi-elliptic extension of the parabolic modeling to account for turbulent contributions to the normal pressure variations, as well as an extension to the turbulence models utilized, to account for the highly enhanced mixing rates observed in situations with large convex curvature. A noniterative, pressure split procedure is shown to extend parabolic models to account for such normal pressure variations in an efficient manner, requiring minimal add...
The linear form of parabolized linear stability equations (PSE) is used in a variational approach t...
A feasibility study was conducted to assess the applicability of an existing parabolic analysis (ADD...
Three different approaches for efficiently computing supersonic flow fields with strong viscous/invi...
Work currently in progress to update an existing transonic circulation control airfoil analysis meth...
The theoretical basis for well posed marching of a Parabolic Navier-Stokes (PNS) computational techn...
Theoretical models are developed and numerical studies conducted on various types of flows including...
A computational model, SCIPVIS, is described which predicts the multiple cell shock structure in imp...
A numerical investigation of incompressible and compressible turbulent flows over strongly curved su...
A direct numerical approach has been developed to simulate supersonic turbulent boundary layers. The...
The compressible Reynolds time averaged Navier-Stokes equations were used to obtain solutions for fl...
A simple theoretical model is proposed to describe the flow of a turbulent wall jet along a curved s...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
This set of analyses involves flow separation in high curvature regions with special attention to ci...
Shock wave turbulent boundary layer interactions (SWTBLI) commonly arise in turbomachinery and aeros...
The authors greatly acknowledge the United Kingdom Turbulence Consortium (UKTC), under EPSRC grant E...
The linear form of parabolized linear stability equations (PSE) is used in a variational approach t...
A feasibility study was conducted to assess the applicability of an existing parabolic analysis (ADD...
Three different approaches for efficiently computing supersonic flow fields with strong viscous/invi...
Work currently in progress to update an existing transonic circulation control airfoil analysis meth...
The theoretical basis for well posed marching of a Parabolic Navier-Stokes (PNS) computational techn...
Theoretical models are developed and numerical studies conducted on various types of flows including...
A computational model, SCIPVIS, is described which predicts the multiple cell shock structure in imp...
A numerical investigation of incompressible and compressible turbulent flows over strongly curved su...
A direct numerical approach has been developed to simulate supersonic turbulent boundary layers. The...
The compressible Reynolds time averaged Navier-Stokes equations were used to obtain solutions for fl...
A simple theoretical model is proposed to describe the flow of a turbulent wall jet along a curved s...
A numerical solution algorithm is established for prediction of subsonic turbulent three-dimensional...
This set of analyses involves flow separation in high curvature regions with special attention to ci...
Shock wave turbulent boundary layer interactions (SWTBLI) commonly arise in turbomachinery and aeros...
The authors greatly acknowledge the United Kingdom Turbulence Consortium (UKTC), under EPSRC grant E...
The linear form of parabolized linear stability equations (PSE) is used in a variational approach t...
A feasibility study was conducted to assess the applicability of an existing parabolic analysis (ADD...
Three different approaches for efficiently computing supersonic flow fields with strong viscous/invi...