The feasibility of the method of lines for solutions of physical problems requiring nonuniform grid distributions is investigated. To attain this, it is also necessary to investigate the stiffness characteristics of the pertinent equations. For specific applications, the governing equations considered are those for viscous, incompressible, two dimensional and axisymmetric flows. These equations are transformed from the physical domain having a variable mesh to a computational domain with a uniform mesh. The two governing partial differential equations are the vorticity and stream function equations. The method of lines is used to solve the vorticity equation and the successive over relaxation technique is used to solve the stream function e...
An approximate axisymmetric method was developed which can reliably calculate fully viscous hyperson...
The stability of a steady, vortical flow in a cylindrical container with one rotating endwall has be...
The interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...
A numerical simulation of the final stages of transition to turbulence in plane channel flow is repo...
Two different viscous-inviscid interaction schemes were developed for the analysis of steady, turbul...
The finite element procedure is shown to be of significant impact in design of the 'computational wi...
A numerical method based on b-spline polynomials was developed to study incompressible flows in cyli...
The design and usage of a pilot program using a finite difference method for calculating the pressur...
An experimental investigation is reported on slanted base ogive cylinders at zero incidence. The Mac...
A finite-difference program is described for calculating the viscous compressible boundary layer flo...
An efficient and accurate method for solving the viscous shock layer equations for hypersonic flows ...
Flow-visualization studies of ogival, parabolic, and conical forebodies were made in a comprehensive...
High-lift system aerodynamics has been gaining attention in recent years. In an effort to improve ai...
Viscous transonic flows at large Reynolds numbers over 3-D wings were analyzed using a zonal viscid-...
A numerical simulation of the final stages of transition to turbulence in plane channel flow at a Re...
An approximate axisymmetric method was developed which can reliably calculate fully viscous hyperson...
The stability of a steady, vortical flow in a cylindrical container with one rotating endwall has be...
The interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...
A numerical simulation of the final stages of transition to turbulence in plane channel flow is repo...
Two different viscous-inviscid interaction schemes were developed for the analysis of steady, turbul...
The finite element procedure is shown to be of significant impact in design of the 'computational wi...
A numerical method based on b-spline polynomials was developed to study incompressible flows in cyli...
The design and usage of a pilot program using a finite difference method for calculating the pressur...
An experimental investigation is reported on slanted base ogive cylinders at zero incidence. The Mac...
A finite-difference program is described for calculating the viscous compressible boundary layer flo...
An efficient and accurate method for solving the viscous shock layer equations for hypersonic flows ...
Flow-visualization studies of ogival, parabolic, and conical forebodies were made in a comprehensive...
High-lift system aerodynamics has been gaining attention in recent years. In an effort to improve ai...
Viscous transonic flows at large Reynolds numbers over 3-D wings were analyzed using a zonal viscid-...
A numerical simulation of the final stages of transition to turbulence in plane channel flow at a Re...
An approximate axisymmetric method was developed which can reliably calculate fully viscous hyperson...
The stability of a steady, vortical flow in a cylindrical container with one rotating endwall has be...
The interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...