Applications
Design of High Performance Pump Stage
Design High Efficiency Impellers with Splitter Blades
Design Optimisation of a Strongly Interacting Diffuser Pump Stage
Design of a Double-Suction Volute Pump
Redesign of an Industrial Compressor Stage
Multi-Objective Optimisation of a Centrifugal Pump Stage by Means of Design of Experiment Coupled with Inverse Design Method
Design High Performance Centrifugal Compressor Impellers
Design of an Automobile Torque Converter
Design of Refrigeration Compressor Stage in R134a
Design of an Inducer Pump with High Suction Performance and Backflow Control
Design High Performance Centrifugal Compressor Vaned Diffusers
Design of a 3 Stage Axial LP Turbine for Aeroengine Applications
Design High Performance Axial Turbine Stages with More Uniform Exit Flow
Design of a Cooling Fan
Design of a Double-Suction Fan Stage
Hydraulic Design Optimisation of a Torque Converter
Publications
- Choice of Optimum Blade Loading in Application of 3D Inverse Design to Design of Pumps and Fans.
- A Compressible Three-Dimensional Design Method for Radial and Mixed Flow Turbomachinery Blades
- On the Role of Three-Dimensional Inverse Design Methods in Turbomachinery Shape Optimization
- Optimization of Pump Blades Using Three Dimensional Inverse Design Method
- Suppression of Secondary Flows in a Mixed-Flow Pump Impeller by Application of Three-Dimensional Inverse Design Method: Part 2 - Experimental Validation
Case Studies
- Design of Mixed Flow Pump Stage Using TURBOdesign1 and CFD Code, Hyosung-Ebara
- Development of New Vertical Line Shaft Pumps
- Improving Turbocharger Centrifugal Compressor Efficiency by TURBOdesign1 - Cummins Turbo
- Design of a Second Stage Hydrogen Rocket Turbopump by TURBOdesign1
- TURBOdesign1 is Extensively Used at Voith Turbo for the Design of Hydrodynamic Torque Converters
On the Design Criteria for Suppression of Secondary Flows in Centrifugal and Mixed Flow Impellers
In this paper, for the first time, a set of guidelines is presented for the systematic design of mixed flow and centrifugal compressors and pumps with suppressed secondary flows and a uniform exit flow field. The paper describes the shape of the optimum pressure distribution for the suppression of secondary flows in the impeller with reference to classical secondary flow theory. The feasibility of achieving this pressure distribution is then demonstrated by deriving guidelines for the design specifications of a three-dimensional inverse design method, in which the blades are designed subject to a specified circulation distribution or 2ττ rVΘ The guidelines will define the optimum choice of the blade loading or δrVΘ /δm and the stacking condition for the blades. These guidelines are then used in the design of three different low specific speed centrifugal pump impellers and a high specific speed industrial centrifugal compressor impellers. The flows through all the designed impellers are computed numerically by a three-dimensional viscous code and the resulting flow field is compared to that obtained in the corresponding conventional impeller. The results show consistent suppression of secondary flows in all cases. The design guidelines are validated experimentally by comparing the performance of the inverse designed centrifugal compressor impeller with the corresponding conventional impeller. The overall performance of the stage with the inverse designed impeller with suppressed secondary flows was found to be 5 percent higher than the conventional impeller at the peak efficiency point. Exit flow traverse results at the impeller exit indicate a more uniform exit flow than that measured at the exit from the conventional impeller.

