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Optimization design of a reversible pump-turbine runner with high efficiency and stability

2015 Frequent changes between pump and turbine operations pose significant challenges in the design of  pump-turbine runners with high efficiency and stability. In this study, a m ...

A Robust Mixing Plane Method and its Application in 3D Inverse Design of Transonic Turbine Stages

Zangeneh, M. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition (Germany) ...

Application of a three-dimensional viscous transonic inverse method to NASA rotor 67

Proc Instn Mech Engrs Vol 216 Part A: J Power and Energy 2002   The development and application of a thre ...

Design of a 3 Stage Axial LP Turbine for Aeroengine Applications

Design Target To develop a high performance 3 stage axial LP turbine in a 6 weeks period time frame to help in a competitive bidding process with other competing aeroengine ...

Application of Simulated Annealing to Inverse Design of Transonic Turbomachinery Cascades

Proc IMechE Vol 216 Part A: J Power and Energy 2002 In turbomachinery blade design, inverse methods and optimizatio ...

Inverse Design of Aeronautical Turbines in Avio S.p.A Design Process

E. Spano Avio S.p.A, Technical Direction, Research Department, Know-how Engineering When Avio S.p.A launch ...

A Fully Compressible Three Dimensional Inverse Design Method Applicable to Radial and Mixed-Flow Turbomachines

Zangeneh, M. Hawthorne, W. R. 1990 A fully three dimensional compres ...

Design of an Hydraulic Turbocharger Pump and Turbine for Reverse Osmosis Desalination Plant Applications

Design Target The scope of this project is the detailed design of a hydraulic turbocharger composed by a Pump and a Radial inflow Turbine for energy recovery in a reverse osm ...

A 3D Inverse Design Based Multidisciplinary Optimization on the Radial and Mixed-Inflow Turbines for Turbochargers

Zangeneh, M. 2014 A methodology for designing radial and mixed-inflow turbines to meet multiple aerodynamic and mec ...

Suppression of Secondary Flows in a Turbine Nozzle with Controlled Stacking Shape and Exit Circulation by 3D Inverse Design Method

International Gas Turbine & Aeroengine Congress & Exhibition 1999   For the axial turbine stage, t ...