Application of an Algorithmically Differentiated Turbomachinery Flow Solver to the Optimization of a Fan Stage
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. Technical University of Kaiserslautern
3. MTU Aero Engines
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3997
Reference43 articles.
1. Overview of Sensitivity Analysis and Shape Optimization for Complex Aerodynamic Configurations
2. Turbomachinery Design Optimization Using Automatic Differentiated Adjoint Code
3. Numerical sensitivity analysis for aerodynamic optimization: A survey of approaches
4. Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines—Part II: Validation and Application
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