CAESES
19 Case Studies
A CAESES Case Study
Technical University of Darmstadt’s Institute of Gas Turbines and Aerospace Propulsion tackled an automated, simultaneous optimization of a vaned diffusor and volute for a centrifugal compressor in collaboration with NUMECA Germany and Kompressorenbau Bannewitz. The challenge was to create a robust, low-parameter CAD workflow for large-scale design exploration; CAESES was used to generate parametric geometry for the volute and non‑axisymmetric diffusor needed for automated variation.
Using CAESES, the team parametrized volute cross-sections and area distribution and the diffusor blade stagger, twist, chord, pitch and rotation, then coupled that geometry to NUMECA meshing and CFD in a fully automated optimization loop targeting isentropic efficiency. The CAESES‑driven process produced a fully automated diffusor–volute optimization with measured gains of 1–4% in isentropic efficiency and 1.45–4.67% increases in total pressure, while revealing the strong influence of the diffusor and additional impact of the volute.
Johannes Ratz
Research Scientist, Institute of Gas Turbines and Aerospace Propulsion