[HTML][HTML] A rotorcraft in-flight ice detection framework using computational aeroacoustics and Bayesian neural networks

M Morelli, J Hauth, A Guardone, X Huan… - Structural and …, 2023 - Springer
This work develops a novel ice detection framework specifically suitable for rotorcraft using
computational aeroacoustics and Bayesian neural networks. In an offline phase of the work …

[HTML][HTML] Aerodynamic shape optimization based on discrete adjoint and RBF

L Abergo, M Morelli, A Guardone - Journal of Computational Physics, 2023 - Elsevier
This paper presents a new framework for Aerodynamic Shape Optimization (ASO)
implemented inside the open-source software SU2. A parametrized surface is iteratively …

Effect of geometric parameters on the noise generated by rod-airfoil configuration

S Sharma, TF Geyer, J Giesler - Applied Acoustics, 2021 - Elsevier
This paper investigates the effect of the geometric parameters–rod diameter and the
distance between the rod and the airfoil–on the noise generated by a rod-airfoil …

On the airfoil leading-edge noise reduction using poro-wavy leading edges

W Chen, H Lei, Y Xing, L Wang, T Zhou, W Qiao - Physics of Fluids, 2024 - pubs.aip.org
This paper presents numerical studies on airfoil leading-edge turbulence interaction noise
reduction using poro-wavy leading edges. Three different bionic treatments including wavy …

Efficient airframe noise reduction framework via adjoint-based shape optimization

BY Zhou, T Albring, NR Gauger, CR da Silva… - AIAA Journal, 2021 - arc.aiaa.org
This paper presents an efficient adjoint-based shape optimization framework for airframe
noise reduction in which algorithmic differentiation (AD) is applied to the open-source …

Extension and Validation of the Turbomachinery Capabilities of SU2 Open Source CFD Code

C Yan, B Wang, X He, F Zhao… - … Expo: Power for …, 2023 - asmedigitalcollection.asme.org
Abstract Computational Fluid Dynamic (CFD) tools have revolutionized the way to design
engineering systems, but most established codes are proprietary and closed-source, making …

Toward adjoint-based aeroacoustic optimization for propeller and rotorcraft applications

RÖ Içke, O Baysal, LV Lopes, BY Zhou… - AIAA Aviation 2020 …, 2020 - arc.aiaa.org
The goal of the present project is to build a multidisciplinary, rapid, robust, and accurate
computational tool to optimize wing-mounted propeller designs. The full Farassat's …

Advances in Intuitive Priors and Scalable Algorithms for Bayesian Deep Neural Network Models in Scientific Applications

J Hauth - 2024 - deepblue.lib.umich.edu
In recent years, deep learning (DL) algorithms have gained widespread use in scientific and
engineering fields, promising insights into complex trends within extensive datasets …

Aerostructural wing shape optimization assisted by algorithmic differentiation

R Bombardieri, R Cavallaro, R Sanchez… - Structural and …, 2021 - Springer
With more efficient structures, last trends in aeronautics have witnessed an increased
flexibility of wings, calling for adequate design and optimization approaches. To correctly …

Towards an open-source framework for aero-structural design and optimization within the su2 suite

R Bombardieri, R Sanchez, R Cavallaro… - Advances in evolutionary …, 2021 - Springer
Ongoing efforts to develop a fully open-source framework for the aero-structural design and
optimization of wings, including aerodynamic and structural geometric nonlinearities, are …