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Recent Articles

Suppression of Secondary Flows in a Mixed-Flow Pump Impeller by Application of Three-Dimensional Inverse Design Method : Part 2

The previous paper describes the design of the blade geometry of a medium specific speed mixed flow pump impeller by using a three-dimensional...

Suppression of Secondary Flows in a Mixed-Flow Pump Impeller by Application of Three-Dimensional Inverse Design Method : Part 1

The paper describes the design of the blade geometry of a medium specific speed mixed flow pump impeller by using a three-dimensional inverse design...

How JAXA, the Japan Aerospace Exploration Agency, Designed their Rocket Engine Turbopump?

At the present time, Stepanoff’s design methodology based on empiricism using an experimental database is still widely used in pump design.

Design of Gas Compressor and LH2Pump Stage for Hydrogen Transport

The global push for decarbonization has inevitably led the world to take a closer look at hydrogen. Hydrogen could be a good option for many sectors...

How to Optimize the Design of a Reversible Pump-Turbine Runner with High Efficiency and Stability?

Pumped hydro energy storage (PHES) is currently the only proven large-scale (>100 MW) energy storage technology. The benefits of PHES on electrical...

Guide to Design a Multi-Stage Pump Inducer

The customer, one of the world’s largest pump manufacturers, asked ADT to design an inducer to fit in one of their products, a multi-stage...

What is the Optimum Blade Loading for Pumps?

Pumps account for 20% of the global energy consumption, and energy is often the largest cost in the life cycle costs of a pump system. Critical to a...

How Hyosung Goodsprings, Pump Leader in Korea, Designed their Mixed Flow Pump Stages?

Hyosung Goodsprings is one of leading pump makers in Korea. We have secured the leading pump maker’s position with the continuous effort over the...

How to Design and Optimize Cryogenic Rocket Engines by Coupling Flownex, TURBOdesign and Ansys Workbench?

As we look at new off-world destinations and applications, our launch-vehicle designs constantly need to evolve. Each component will need to be...

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