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Design of a Mixed-Flow Transonic Compressor for Active High-Lift System using 3D Inverse Design

Written by Dr. Peng Wang, Maria Vera-Morales, Patrick La and Prof. Mehrdad Zangeneh from Advanced Design Technology, Niklas Maroldt, Ole Willers, Felix Kauth, Jorg Seume from Institute of Turbomachinery and Fluid Dynamics, Leibniz Universitat Hannover.

What's inside?

This paper was presented at the 2020 ASME Turbo Expo and explores the redesign of an electrically driven, mixed-flow transonic compressor by using a 3D Inverse Design Methodology. This work was done as part of a collaboration with the Liebniz University Hannover.

The advantage of using an inverse design methodology is shown in this paper as a method that allows a very simple parameterization, reducing significantly the design time and hence allowing the exploration of wider design spaces, with the potential of reaching more innovative and efficient designs.

 

Design Mixed Flow Transonic Compressor for Active High-Lift System Cover


The flow field analysis revealed that the improvement by inverse design was due to the reduction of stagnation and secondary flow in the rotor and the mitigation of the flow separation in the stator's hub section.

In this publication, you will:

  1. Discover a fast and reliable 3D Inverse Design method that plays an important role in developing aircraft electrification.
  2. Understand the stringent size and operational constraints of the compressor in a high-lift system.
  3. See the simplified design process and how an inverse design approach shortens the design time and allows for a much wider exploration of the design space.
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