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In this paper the further enhancement of the 3D viscous transonic inverse design code TURBOdesign-2 and its application to the re-design of NASA37 and NASA67 rotors will be described.

The application of the method is explored using a transonic test case, NASA rotor 67. From an understanding of the dynamics of the flow in the fan in relation to its pressure loading distributions, simple guidelines can be developed for the inverse method in
order to weaken the shock formation.

The Japan Aerospace Exploration Agency used TURBOdesign Suite to overcome 'Stepanoff's Spell' in pump design and create a rocket engine turbopump with compact size and high efficiency.

CREMHyG used TURBOdesign Suite to design the components for a hydrogen rocket turbopump, including a very complex return channel.

ADT engineers carried out a project to optimize a fuel pump impeller for cavitation and efficiency. The main challenge was to meet targets at multiple operating conditions.

This webinar presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D inverse design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall and thus contributing to the reduction of both the aircraft noise footprint and the impact of aviation emission on local air quality.

This paper presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D Inverse Design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall.

In this work, the redesign of a centrifugal transonic compressor impeller with splitter blades by means of the three-dimensional inverse design code TURBOdesign-1 is presented.

A defence contractor used TURBOdesign Suite to bring their fan design process in-house to reduce development time and cost.