Adjoint formulation of a steady multistage turbomachinery interface using automatic differentiation
Author:
Funder
FCT
Publisher
Elsevier BV
Subject
General Engineering,General Computer Science
Reference29 articles.
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1. A review on aerodynamic optimization of turbomachinery using adjoint method;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2024-01-23
2. Uncertainty Quantification of Compressor Map Using the Monte Carlo Approach Accelerated by an Adjoint-Based Nonlinear Method;Aerospace;2023-03-11
3. Continuous adjoint‐based shape optimization of a turbomachinery stage using a 3D volumetric parameterization;International Journal for Numerical Methods in Fluids;2023-02-17
4. Adjoint-based shape sensitivity of multi-row turbomachinery;Structural and Multidisciplinary Optimization;2019-08-31
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