Abstract: A numerical algorithm for three-dimensional compressible inviscid subsonic flows is presented. The steady-state solution is obtained as a limit of time-stepping procedure. The conservation equations of gasdynamics are written in curvilinear coordinates. The method of alternating directions is implemented for solving difference equations. For one of the directions the implicit scheme is used. The numerical results for the flow about a sphere for several Mach numbers are presented.Note: Research direction:Mathematical modelling in actual problems of science and technic
Title: Numerical Solution of the Three-dimensional Compressible Flow Author: Martin Kyncl Department...
The basic idea of pressure based method to predict compressible flows solving the governing partial ...
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...
In this study a Computational Fluid Dynamics (CFD) code to solve the two-dimensional subsonic flow a...
Abstract: The algorithm for numerical simulation of subsonic flows over complex shaped bod...
The most important methods used in obtaining solutions to compressible flow around bodies at subsoni...
The flow of the compressible gas is investigated by means of the developed finite-difference compute...
The three-dimensional ideal gas flow in the shock layer of a blunted supersonic cone at an angle of ...
This work deals with a numerical simulation of 2D and 3D inviscid and laminar compressible flows aro...
Abstract:-The unsteady and inviscid compressible flow around a circular cylinder and airfoil has bee...
Recent progress in the development of robust and accurate discretization methods for the compressibl...
The overall objective of the research carried out over the last two years was the development of new...
An integral method, previously used to obtain compressible flow past two-dimensional shapes, is appl...
A comprehensive computational procedure is presented for predicting the supersonic region of the flo...
An implicit, space-marching, finite-difference procedure is presented for solving the primitive vari...
Title: Numerical Solution of the Three-dimensional Compressible Flow Author: Martin Kyncl Department...
The basic idea of pressure based method to predict compressible flows solving the governing partial ...
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...
In this study a Computational Fluid Dynamics (CFD) code to solve the two-dimensional subsonic flow a...
Abstract: The algorithm for numerical simulation of subsonic flows over complex shaped bod...
The most important methods used in obtaining solutions to compressible flow around bodies at subsoni...
The flow of the compressible gas is investigated by means of the developed finite-difference compute...
The three-dimensional ideal gas flow in the shock layer of a blunted supersonic cone at an angle of ...
This work deals with a numerical simulation of 2D and 3D inviscid and laminar compressible flows aro...
Abstract:-The unsteady and inviscid compressible flow around a circular cylinder and airfoil has bee...
Recent progress in the development of robust and accurate discretization methods for the compressibl...
The overall objective of the research carried out over the last two years was the development of new...
An integral method, previously used to obtain compressible flow past two-dimensional shapes, is appl...
A comprehensive computational procedure is presented for predicting the supersonic region of the flo...
An implicit, space-marching, finite-difference procedure is presented for solving the primitive vari...
Title: Numerical Solution of the Three-dimensional Compressible Flow Author: Martin Kyncl Department...
The basic idea of pressure based method to predict compressible flows solving the governing partial ...
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...