A review and comparison of error estimators for anisotropic mesh adaptation for flow simulations

A Balan, MA Park, SL Wood, WK Anderson… - Computers & …, 2022 - Elsevier
Automated mesh adaptation is known to be an efficient way to control discretization errors in
Computational Fluid Dynamics (CFD) simulations. It offers the added advantage that the …

Developing the orthotropic linear-elastic model for wood applications using the FE method

T Chakkour, P Perré - Materials Advances, 2024 - pubs.rsc.org
The purpose of this work is to develop the three-dimensional (3D) finite element (FE)
modeling approach for the linear mechanical behavior of the wood material. The developed …

Wall-Modeled Large-Eddy Simulation Method for Unstructured-Grid Navier–Stokes Solvers

L Wang, WK Anderson, EJ Nielsen, PS Iyer… - Journal of Aircraft, 2024 - arc.aiaa.org
This paper reports on the implementation and assessment of a wall-modeled large-eddy
simulation (WMLES) methodology in an unstructured-grid, node-centered flow solver …

Flutter Analysis with Stabilized Finite Elements based on the Linearized Frequency-domain Approach

K Jacobson, B Stanford, S Wood… - AIAA SciTech 2020 …, 2020 - arc.aiaa.org
When designing and certifying aircraft, engineers must take into consideration aeroelastic
effects such as flutter. Design and certification of a vehicle may require analysis of …

Exploring Unstructured Mesh Adaptation for Hybrid Reynolds-Averaged Navier–Stokes/Large Eddy Simulation

MA Park, WL Kleb, WK Anderson, SL Wood… - AIAA SciTech 2020 …, 2020 - arc.aiaa.org
Mesh adaptation methods for the Reynolds-averaged Navier–Stokes (RANS) equations are
rapidly maturing and beginning to impact the design of aerospace vehicles. RANS …

Verification of anisotropic mesh adaptation for complex aerospace applications

A Balan, MA Park, S Wood, WK Anderson - AIAA scitech 2020 forum, 2020 - arc.aiaa.org
The stabilized finite element solver, FUN3D-SFE, along with the grid mechanics
package\refine are verified for aerospace applications of laminar and turbulent flow …

Aeroelastic Analysis of Highly Flexible Wings with Linearized Frequency-Domain Aerodynamics

BK Stanford, KE Jacobson, P Chwalowski - Journal of Aircraft, 2024 - arc.aiaa.org
Aeroelastic flutter analysis of configurations with geometric structural nonlinearities typically
is done with time-domain analysis. The results from this process are computationally …

Massive parallelization and performance enhancement of an immersed boundary method based unsteady flow solver

R Sundar, D Majumdar, CL Shah, S Sarkar - arXiv preprint arXiv …, 2024 - arxiv.org
High-fidelity simulations of unsteady fluid flow are now possible with advancements in high-
performance computing hardware and software frameworks. Since computational fluid …

Flutter-Constrained Optimization with the Linearized Frequency-Domain Approach

K Jacobson, B Stanford - AIAA SciTech 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-2242. vid Due to the high
computational cost associated with unsteady aeroelastic analysis, state-of-the-art …

Anisotropic goal-based mesh adaptation metric clarification and development

DS Kamenetskiy, JA Krakos, TR Michal… - AIAA SCITECH 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1245. vid Adaptive unstructured
mesh techniques have a limited, but growing impact on production analysis workflows to …