This thesis studies steady, two dimensional flow of an inviscid, incompressible fluid over an arbitrary symmetric profile. Flows with zero and variable vorticity are considered. In the present work a numerical algorithm is given for a class of lows that can also be solved by perturbation techniques. However, reliable solutions by the perturbation technique, especially in the case of rotational flows, require complicated analytical methods even in the case of the circle. Thus, one of the goals of this thesis is to provide a fast and efficient algorithm from which a solution to several standard problems can be obtained with less effort. The equations of motion based on a transformation of coordinate systems are derived. The approach is new in...
Finite Spectral QUICK scheme is developed to calculate incompressible viscous flows. This scheme is ...
We present a class of a high-resolution Godunov-type algorithms for solving flow problems governed b...
In this method the inviscid flow field is decomposed into two parts: a known field with constant vor...
This dissertation studies steady two-dimensional transonic flows past symmetric airfoils. The flow e...
Various forms of FP (full potential) equation, spatial differencing schemes, and iterative schemes a...
Numerical solutions are obtained for two-dimensional incompressible turbulent viscous flow over airf...
This thesis proposes and examines various algorithms for analysis of steady ideal fluid capillary fl...
Abstract: As well known the solution of the incompressible flow problem in a double-connec...
Abstract. The work deals with a numerical solution of 2D steady and unsteady inviscid incom-pressibl...
Transonic flow past ellipsoids of revolution at zero incidence has been solved assuming the flow to ...
A numerical solution is presented for the incompressible flow over thin planar and axisymmetric prof...
In this paper we discuss a novel accurate method for computing transonic flow over lifting and non-l...
A curvilinear coordinate system $x\sp{i}$ has been introduced to study 2 $-$ D flow in complex geome...
We present a general procedure to construct a non-linear mimetic finite-difference operator. The me...
An existing iterative implicit flow solver based on direct divergence-linked pressure correction is ...
Finite Spectral QUICK scheme is developed to calculate incompressible viscous flows. This scheme is ...
We present a class of a high-resolution Godunov-type algorithms for solving flow problems governed b...
In this method the inviscid flow field is decomposed into two parts: a known field with constant vor...
This dissertation studies steady two-dimensional transonic flows past symmetric airfoils. The flow e...
Various forms of FP (full potential) equation, spatial differencing schemes, and iterative schemes a...
Numerical solutions are obtained for two-dimensional incompressible turbulent viscous flow over airf...
This thesis proposes and examines various algorithms for analysis of steady ideal fluid capillary fl...
Abstract: As well known the solution of the incompressible flow problem in a double-connec...
Abstract. The work deals with a numerical solution of 2D steady and unsteady inviscid incom-pressibl...
Transonic flow past ellipsoids of revolution at zero incidence has been solved assuming the flow to ...
A numerical solution is presented for the incompressible flow over thin planar and axisymmetric prof...
In this paper we discuss a novel accurate method for computing transonic flow over lifting and non-l...
A curvilinear coordinate system $x\sp{i}$ has been introduced to study 2 $-$ D flow in complex geome...
We present a general procedure to construct a non-linear mimetic finite-difference operator. The me...
An existing iterative implicit flow solver based on direct divergence-linked pressure correction is ...
Finite Spectral QUICK scheme is developed to calculate incompressible viscous flows. This scheme is ...
We present a class of a high-resolution Godunov-type algorithms for solving flow problems governed b...
In this method the inviscid flow field is decomposed into two parts: a known field with constant vor...