Continuous adjoint methods for turbulent flows, applied to shape and topology optimization: industrial applications

EM Papoutsis-Kiachagias… - Archives of Computational …, 2016 - Springer
This article focuses on the formulation, validation and application of the continuous adjoint
method for turbulent flows in aero/hydrodynamic optimization. Though discrete adjoint has …

[HTML][HTML] Adjoint-based fluid dynamic design optimization in quasi-periodic unsteady flow problems using a harmonic balance method

A Rubino, M Pini, P Colonna, T Albring… - Journal of …, 2018 - Elsevier
Shape optimization in unsteady flow problems enables the consideration of dynamic effects
on design. The ability to treat unsteady effects is attractive, as it can provide performance …

Proper orthogonal decomposition assisted inverse design optimisation method for the compressor cascade airfoil

Y Zhu, Y Ju, C Zhang - Aerospace Science and Technology, 2020 - Elsevier
Inverse design is by far the most physically explicit method in the turbomachinery field for
designing a cascade airfoil shape for a prescribed distribution of aerodynamic parameters …

An efficient unsteady adjoint optimization system for multistage turbomachinery

C Ma, X Su, X Yuan - Journal of Turbomachinery, 2017 - asmedigitalcollection.asme.org
Unsteady blade row interactions play an important role in the performance of multistage
turbomachinery. However, most aerodynamic optimizations of multistage turbomachinery …

[HTML][HTML] Fully-turbulent adjoint method for the unsteady shape optimization of multi-row turbomachinery

A Rubino, S Vitale, P Colonna, M Pini - Aerospace Science and …, 2020 - Elsevier
The possibility of taking into account unsteady flow effects if performing turbomachinery
shape optimization is attractive to accurately address inherently time dependent design …

Deep learning based adaptive deformation of aerodynamic shape for ducted propellers

L Liu, T Wang, Z Gao, L Zeng, X Shao - Aerospace Science and …, 2023 - Elsevier
Ducted propellers are widely used in eVTOL. The leading edge shape of the duct plays an
important role in the aerodynamic performance of the ducted propeller. In this work, an …

A review on aerodynamic optimization of turbomachinery using adjoint method

R Lavimi, AE Benchikh Le Hocine… - Proceedings of the …, 2024 - journals.sagepub.com
Improvements in aerodynamic turbomachinery design have gained attraction due to the
increased demand for a more sustainable future. Several optimization approaches have …

Fully implicit discrete-adjoint methods for rotorcraft applications

M Biava, M Woodgate, GN Barakos - AIAA Journal, 2016 - arc.aiaa.org
This paper presents the development of a fully implicit, low-memory discrete-adjoint method
by means of automatic source-code differentiation applied to the Helicopter Multi-Block …

Non-iterative generation of an optimal mesh for a blade passage using deep reinforcement learning

I Kim, S Kim, D You - Computer Physics Communications, 2024 - Elsevier
A method using deep reinforcement learning (DRL) to non-iteratively generate an optimal
mesh for an arbitrary blade passage is developed. Despite automation in mesh generation …

Radial turbine optimization under unsteady flow using nature-inspired algorithms

S Mehrnia, K Miyagawa, J Kusaka… - Aerospace Science and …, 2020 - Elsevier
This paper investigated the performance of a radial flow turbine by coupling metaheuristic
algorithms with Computational Fluid Dynamics. We performed the optimization of the casing …