A review on design of experiments and surrogate models in aircraft real-time and many-query aerodynamic analyses

R Yondo, E Andrés, E Valero - Progress in aerospace sciences, 2018 - Elsevier
Full scale aerodynamic wind tunnel testing, numerical simulation of high dimensional (full-
order) aerodynamic models or flight testing are some of the fundamental but complex steps …

A review of surrogate modeling techniques for aerodynamic analysis and optimization: current limitations and future challenges in industry

R Yondo, K Bobrowski, E Andrés, E Valero - Advances in evolutionary and …, 2019 - Springer
Recent progresses in aircraft aerodynamics have witnessed the introduction of surrogate-
based approaches in design analysis and optimization as an alternative to address the …

[HTML][HTML] An airfoil optimization technique for wind turbines

AFP Ribeiro, AM Awruch, HM Gomes - Applied Mathematical Modelling, 2012 - Elsevier
Optimization algorithms coupled with computational fluid dynamics are used for wind
turbines airfoils design. This differs from the traditional aerospace design process since the …

Optimal design of aeroacoustic airfoils with owl-inspired trailing-edge serrations

M Zhao, H Cao, M Zhang, C Liao… - Bioinspiration & …, 2021 - iopscience.iop.org
The trailing-edge serration that imitates the silent owl wing is used as a flow control method
to suppress the aerodynamic noise generated from the rotating wind turbine blade. Recent …

A new optimization approach to improve the overall performance of thick wind turbine airfoils

X Li, K Yang, J Bai, J Xu - Energy, 2016 - Elsevier
A crucial problem of designing thick airfoils is balancing structural and aerodynamic
requirements. This paper documented a new idea to deal with the thick airfoil's design …

[HTML][HTML] Robust and efficient adjoint solver for complex flow conditions

S Xu, S Timme - Computers & Fluids, 2017 - Elsevier
A key step in gradient-based aerodynamic shape optimisation using the Reynolds-averaged
Navier–Stokes equations is to compute the adjoint solution. Adjoint equations inherit the …

Wing-body junction optimisation with CAD-based parametrisation including a moving intersection

S Xu, S Timme, O Mykhaskiv, JD Müller - Aerospace Science and …, 2017 - Elsevier
Over the past decades significant progress has been made with adjoint computational fluid
dynamics solvers, which are an essential part of efficient high-fidelity aerodynamic shape …

Multidisciplinary optimization of an NLF forward swept wing in combination with aeroelastic tailoring using CFRP: DLR contribution to the LuFo IV joint research …

T Wunderlich, S Dähne, L Heinrich… - CEAS Aeronautical Journal, 2017 - Springer
This article introduces a process chain for commercial aircraft wing multidisciplinary
optimization (MDO) based on high fidelity simulation methods. The architecture of this …

Relaxed gradient projection algorithm for constrained node-based shape optimization

I Antonau, M Hojjat, KU Bletzinger - Structural and Multidisciplinary …, 2021 - Springer
In node-based shape optimization, there are a vast amount of design parameters, and the
objectives, as well as the physical constraints, are non-linear in state and design. Robust …

Multidisciplinary wing optimization of commercial aircraft with consideration of static aeroelasticity

TF Wunderlich - CEAS Aeronautical Journal, 2015 - Springer
This article presents the development and application of a high-fidelity simulation process
chain for commercial aircraft wing multidisciplinary optimization. Based upon a parametric …