This research describes the development of a new structured 2D CFD solver for compressible flow. The high-speed turbulent flow in a diffuser and a cascade of nozzle blade are predicted using standard k-e turbulence model. The new finite volume CFD solver employs second order accurate central differencing scheme for spatial discretization and multi-stage Runge-Kutta time integration to solve the set of non-linear governing equations with variables stored at the vertices. Artificial dissipations with pressure sensors are introduced to control solution stability and capture shock discontinuity. In general, the predictions compare well with the experimental measurements
Abstract. This work deals with a numerical simulation of 2D inviscid and laminar compressible flows ...
An implicit procedure based on the artificial compressibility formulation is presented for the numer...
This work deals with a numerical simulation of 2D and 3D inviscid and laminar compressible flows aro...
Abstract: This research describes the development of a new structured 2D CFD solver for compressible...
This research describes the development of a new structured 2D CFD solver for compressible flow. The...
The present thesis describes the development of a computational method for the numerical simulation ...
The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outfl...
The thrust produced by a rocket motor is mainly dependent upon the expansion of the product gases th...
Computational fluid dynamics can be used to gain deeper insight into compressible flow physics, but ...
Results are presented for finite element computations involving high speed, viscous compressible int...
As a part of the Dutch ISNaS project our group and NLR jointly develop a flow solver for compressibl...
Four time-dependent numerical algorithms for the prediction of unsteady, viscous compressible flows ...
The basic idea of pressure based method to predict compressible flows solving the governing partial ...
This work deals with a numerical simulation of 2D inviscid and laminar compressible flows in the DCA...
A block structured compressible flow solver based on a finite volume approach with central spatial d...
Abstract. This work deals with a numerical simulation of 2D inviscid and laminar compressible flows ...
An implicit procedure based on the artificial compressibility formulation is presented for the numer...
This work deals with a numerical simulation of 2D and 3D inviscid and laminar compressible flows aro...
Abstract: This research describes the development of a new structured 2D CFD solver for compressible...
This research describes the development of a new structured 2D CFD solver for compressible flow. The...
The present thesis describes the development of a computational method for the numerical simulation ...
The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outfl...
The thrust produced by a rocket motor is mainly dependent upon the expansion of the product gases th...
Computational fluid dynamics can be used to gain deeper insight into compressible flow physics, but ...
Results are presented for finite element computations involving high speed, viscous compressible int...
As a part of the Dutch ISNaS project our group and NLR jointly develop a flow solver for compressibl...
Four time-dependent numerical algorithms for the prediction of unsteady, viscous compressible flows ...
The basic idea of pressure based method to predict compressible flows solving the governing partial ...
This work deals with a numerical simulation of 2D inviscid and laminar compressible flows in the DCA...
A block structured compressible flow solver based on a finite volume approach with central spatial d...
Abstract. This work deals with a numerical simulation of 2D inviscid and laminar compressible flows ...
An implicit procedure based on the artificial compressibility formulation is presented for the numer...
This work deals with a numerical simulation of 2D and 3D inviscid and laminar compressible flows aro...