The design and optimization of a multistage radial compressor vaneless diffuser, cross-over
and return channel is presented. An analytical design procedure for 3D blades with …

The goal of this project is to report on some computational investigations about the return
flow passages. The return flow channel provides the connection and carries the flow …

The goal of this project is to develop a new simplified computational method by means of 2D
approach to determine the 3D axial compressor rotor performance map. Hence, an inviscid …

In this project a new computational code is developed using cell centered finite volume
method with constant space-wise approximation over a control volume to solve the Euler …

The design and optimisation of a vaneless diffuser, cross-over and return channel of a
multistage radial compressor is presented. Special attention is given to the extension of the …