Topology optimization for unsteady flow

S Kreissl, G Pingen, K Maute - International Journal for …, 2011 - Wiley Online Library
A computational methodology for optimizing the conceptual layout of unsteady flow
problems at low Reynolds numbers is presented. The geometry of the design is described …

Multiscale design optimization of lithium ion batteries using adjoint sensitivity analysis

S Golmon, K Maute, ML Dunn - International Journal for …, 2012 - Wiley Online Library
The capacity of lithium ion batteries can be improved through the use of functionally graded
electrodes. Here, we present a computational framework for optimizing the layout of …

Adjoint-based optimization for understanding and suppressing jet noise

JB Freund - Journal of Sound and Vibration, 2011 - Elsevier
Advanced simulation tools, particularly large-eddy simulation techniques, are becoming
capable of making quality predictions of jet noise for realistic nozzle geometries and at …

Sensitivity analysis of limit cycle oscillations

JA Krakos, Q Wang, SR Hall, DL Darmofal - Journal of Computational …, 2012 - Elsevier
Many unsteady problems equilibrate to periodic behavior. For these problems the sensitivity
of periodic outputs to system parameters are often desired, and must be estimated from a …

Optimizing Proprotor Blades Using Coupled Aeroacoustic and Aerodynamic Sensitivities

RÖ Içke, O Baysal, LV Lopes, B Diskin - AIAA Aviation 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3037. vid A quieter and
aerodynamically more efficient proprotor design requires high-fidelity and well-integrated …

On-the-Fly Unsteady Adjoint Aerodynamic and Aeroacoustic Optimization Method

H Zhi, T Xiao, N Qin, S Deng, Z Lu - AIAA Journal, 2024 - arc.aiaa.org
An on-the-fly unsteady adjoint-based aerodynamic and aeroacoustic optimization
methodology is presented, aiming to achieve practical engineering applications to explore …

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 …

Effect of small-scale output unsteadiness on adjoint-based sensitivity

JA Krakos, DL Darmofal - AIAA journal, 2010 - arc.aiaa.org
WITH its roots in the calculus of variations, adjoint analysis has long been used in optimal
control theory (as a reference, see Bryson and Ho [1]) and in weather model tuning [2–4]. Its …

[PDF][PDF] Lattice Boltzmann topology optimization for transient flow

A Kirk, S Kreissl, G Pingen, K Maute - MAESC 2011 Conference May, 2011 - academia.edu
A computational design methodology for transient fluid flows is introduced, using gradient-
based topology optimization. The approach builds on the authors' previous work on steady …

[PDF][PDF] Finite element modeling and optimization of high-speed aerothermoelastic systems

MA Howard - Ph. D. Thesis, 2010 - scholar.colorado.edu
The design of modern aerospace structures that are capable of flying at hypersonic speeds
requires not only careful analysis of the relevant individual physical phenomena, for …