ADT will demonstrate the TURBOdesign Suite and its three-dimensional (3D) inverse design optimization capabilities for Multidisciplinary Optimization of a High-Speed Low Pressure Turbine Rotor and A Novel Optimisation of a Transonic Centrifugal Impeller. Design engineers and original equipment manufacturers can benefit by shortening development times and improving components efficiency using the TURBOdesign Suite and ADT’s engineering design services.
Date: Monday, June 26, 8:00 AM (EDT)
Authors: Dr. Luying Zhang (Advanced Design Technology Ltd) and Prof. Mehrdad Zangeneh (University College London)
Date: Tuesday, June 27, 8:00 AM (EDT)
Authors: Peng Wang and Mingding Zhang (Advanced Design Technology Ltd) and Prof. Mehrdad Zangeneh (University College London)
The process of defining the shape of a centrifugal impeller's blade is crucial for optimizing its performance. It often requires multiple control parameters to accurately represent the blade profile with the desired level of detail and smoothness.
However, as the number of parameters increases, the optimization process becomes increasingly complex, requiring significant computational resources and time.
While textbooks offer design methods and guidelines, the real challenge lies in achieving accurate, quick, and cost-effective optimization for product development, especially when targeting multiple operating conditions.
This paper presents a new design and optimization strategy that combines the 3D inverse approach with a Design of Experiment (DoE) study. The proposed method is applied to redesign and optimize a well-known transonic centrifugal compressor.
Computational Fluid Dynamics (CFD) analysis confirms that the efficiency of the redesigned compressor wheel is significantly improved across the entire performance range. Detailed visualization of the internal flow also shows that reducing leakage loss is crucial in this improvement.
Significantly, the computational time for the CFD simulations is reduced to just a few days on a 32-core computer, as opposed to weeks. The methodology presented in this study can be easily extended to different types of turbomachinery.
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