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Publications / Basic Theory

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Read the latest and previous editions of our publications on Basic Theory in our library.

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

A fully three-dimensional inverse design method for the design of radial and mixed flow turbomachines is described. 

Development of An (Adaptive) Unstructured 2-D Inverse Design Method for Turbomachinery Blade

An aerodynamics inverse design method for turbomachinery blades using fully (adaptive) unstructured meshes is presented. In this design method, the pressure loading (i.e. pressure jump across the blades) and thickness distribution are prescribed.

Three-Dimensional Automatic Optimization Method for Turbomachinery Blade Design

In deriving automatic numerical optimization algorithms for aerodynamic applications, it is quite important to choose a suitable cost function and a suitable set of design parameters. The unknown air foil/blade proŽ les are usually chosen tobe thedesign parameters.

On the Role of Three-Dimensional Inverse Design Methods in Turbomachinery Shape Optimization

The application of a three-dimensional (3D) inverse design method in which the blade geometry is computed for a specified distribution of circulation to the design of turbomachinery blades is explored by using two examples. 

On The Simultaneous Design of Blade and Duct Geometry of Marine Ducted Propulsors

A fully three-dimensional compressive inverse design method for the design of radial and mixed flow turbomachines is described. 

A 3D Automatic Optimization Strategy for Design of Centrifugal Compressor Impeller Blades

In deriving automatic numerical optimization algorithms for aerodynamic applications, the design parameters are usually chosen to be the unknown airfoil/blades profiles. 

On the Inverse Design of Inter-stage Ducts, Diffuser Walls and Meridional Geometry of Turbomachines

In deriving automatic numerical optimization algorithms for aerodynamic applications, the design parameters are usually chosen to be the unknown airfoil/blades profiles. 

Development of A 3D Inverse Design Code for Application to Different Turbo and Hydraulic Machinery Components

A method is presented for the design of multi-component marine ducted propulsors of arbitrary blades loading operating in axisymmetric shear flow.

A Method for the Inverse Design of Ducted Propulsors Operating in Axisymmetric Shear Flows

Since the concept was first developed earlier this century marine ducted propulsors have been installed on vessels ranging from tugs and trawlers through to super-tankers, submarines and torpedoes. 

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