Abstract
The paper is aimed to describe the robust optimization process for a shape optimization of a low pressure turbine (LPT) guide vane cluster. The multidisciplinary analysis, needed to evaluate multidisciplinary constraints, which drive the vane cluster design, is described. Attention is paid to the different sources of uncertainty, such as manufacturing tolerances, material parameters and performance parameters. An overview of the recent methods for the Reliability-based Robust Design Optimization (RBRDO) is presented, with the focus on efficient adaptive surrogate-based method. Finally, a new surrogate-based approach is introduced, which is inspired by the Efficient Global Optimization (EGO) method1 and inverse reliability analysis.
| Original language | English |
|---|---|
| Title of host publication | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624103681 |
| State | Published - 2015 |
| Event | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015 - Dallas, United States Duration: 22 Jun 2015 → 26 Jun 2015 |
Publication series
| Name | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference |
|---|
Conference
| Conference | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015 |
|---|---|
| Country/Territory | United States |
| City | Dallas |
| Period | 22/06/15 → 26/06/15 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 9 Industry, Innovation, and Infrastructure
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