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Recent Articles

Optimize Axial Fan Design Using Inverse Design

In this post we look at designing an axial fan by the 3D Inverse Design method. The entire design process includes controlling the blade loading to...

3DLab and Optima to Export Geometries into Desired CFD Tools using TURBOdesign v6.4

In TURBOdesign v6.4 3DLab - A new export of geometries capability has been added to generate and partition flow domains and facilitate the...

New TURBOdesign Suite module for integration with STAR-CCM+

TURBOdesign Link-CCM+ is a new application which allows integration of TURBOdesign Optima, TURBOdesign1, TURBOdesign 3DLab and STAR-CCM+. The new...

M4 Generic Method for Meridional Geometry Parameterization

The version 6.4 update to TURBOdesign Suite provides significant new features and functionality to enable designers to produce highly optimised...

Introducing TURBOdesign Suite v6.4 for turbomachinery design and optimization

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

A robust mixing plane method satisfying interface flux conservation, nonreflectivity and retaining interface flow variation; valid at all Mach...

ADT presents TURBOdesign Technology at 14th AICFM Conference 2017

Mehrdad Zangeneh (Managing Director) and Peng Wang (Turbomachinery Design Engineer) of Advanced Design Technology (ADT) attended the 14th Asian...

Global TURBOdesign Symposium Highlights

Advanced Design Technology (ADT) hosted their Global TURBOdesign Symposium on Monday 6th and Tuesday 7th November at the Holiday Inn Bloomsbury,...

What is blade loading and how is it specified?

Blade loading is the single most important aerodynamic design parameter in turbomachinery blades. It defines the amount of work made or extracted by...

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