Browse our Turbines Publications
Read the latest and previous editions of our publications on Turbines in our library.
Most radial turbines have a peak efficiency at around U/Cis (velocity ratio or jet speed ratio) of 0.7. It is a well-known fact that it is beneficial for radial turbocharger turbines to have a higher efficiency at low U/Cis region.
An Inverse Design Based Methodology for Rapid 3D Multi-Objective / Multi-Disciplinary Optimisation of Axial Turbines
Design of axial turbines, especially LP turbines, poses difficult tradeoffs between requirements of aerodynamic design and structural limitations.
Optimization of Microturbine Aerodynamics Using CFD, Inverse Design and FEM Structural Analysis (2nd Report:Turbine Design)
In this second report, a new aerodynamic design is presented for a radial turbine stage of a microturbine engine.
Suppression of Secondary Flows in a Turbine Nozzle with Controlled Stacking Shape and Exit Circulation by 3D Inverse Design Method
For the axial stage, the design of circulation distribution between the nozzle and blade has an important effect on the stage performance, because it determines the work distribution in the blade, the stage reaction and the twisting shape of the blade.