Oscar A. Mariño

ORCID: 0000-0003-3143-3813
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About
Contact & Profiles
Research Areas
  • Aerodynamics and Acoustics in Jet Flows
  • Computational Fluid Dynamics and Aerodynamics
  • Fluid Dynamics and Turbulent Flows
  • Acoustic Wave Phenomena Research
  • Model Reduction and Neural Networks
  • Advanced Numerical Methods in Computational Mathematics
  • Wind and Air Flow Studies
  • Wind Turbine Control Systems
  • Energy Load and Power Forecasting
  • Smart Grid Energy Management
  • Lattice Boltzmann Simulation Studies
  • Vehicle Noise and Vibration Control
  • Fluid Dynamics and Vibration Analysis
  • Geography and Education Methods
  • Combustion and Detonation Processes
  • Numerical methods for differential equations
  • Image and Signal Denoising Methods
  • Iterative Learning Control Systems
  • Educational theories and practices
  • Wind Energy Research and Development
  • Neural Networks and Applications
  • Advanced Multi-Objective Optimization Algorithms
  • Advanced Control Systems Optimization
  • Building Energy and Comfort Optimization
  • Fire dynamics and safety research

Universidad Politécnica de Madrid
2022-2024

Universidad de Los Andes
2020

We present the latest developments of our High-Order Spectral Element Solver (), an open source high-order discontinuous Galerkin framework, capable solving a variety flow applications, including compressible flows (with or without shocks), incompressible flows, various RANS and LES turbulence models, particle dynamics, multiphase aeroacoustics. provide overview spatial discretisation (including energy/entropy stable schemes) anisotropic p-adaptation capabilities. The solver is parallelised...

10.1016/j.cpc.2023.108700 article EN cc-by Computer Physics Communications 2023-02-24

Aeroacoustic noise is a major concern in wind turbine design that can be minimized by optimizing the airfoils shape rotating blades. To this end, we present framework for airfoil optimization to reduce trailing edge of Far-field evaluated using Amiet's theory coupled with TNO-Blake model calculate wall pressure spectrum and fast turn-around XFOIL simulations evaluate boundary layer parameters. The computational first validated NACA0012 at 0° angle attack. Particle swarm used find optimized...

10.1016/j.eswa.2023.119513 article EN cc-by-nc-nd Expert Systems with Applications 2023-01-13

We propose an invariant feature space for the detection of viscous dominated and turbulent regions (i.e., boundary layers wakes). The developed methodology uses principal invariants strain rotational rate tensors as input to unsupervised Machine Learning Gaussian mixture model. selected is independent coordinate frame used generate processed data, it relies on rate, which are Galilean invariants. This allows us identify two distinct flow regions: a dominated, region (boundary layer wake...

10.1063/5.0138626 article EN Physics of Fluids 2023-01-21

Abstract. The growing demand for offshore wind energy has led to a significant increase in turbine size and the development of large-scale farms, often comprising 100 150 turbines. However, environmental impact underwater noise emissions remains largely unaddressed. This paper quantifies, first time, aerodynamic footprint three large turbines (5 MW, 10 22 MW) farms composed these We propose novel methodology that integrates validated prediction techniques with plane wave propagation theory...

10.5194/wes-2025-40 preprint EN cc-by 2025-04-07

Aerodynamic noise is a limitation for further exploitation of wind energy resources. As this type caused by the interaction turbulent flow with airframe, detailed resolution necessary to obtain an accurate prediction far-field noise. Computational fluid dynamic (CFD) solvers simulate field but only at high computational cost, which much increased when acoustic resolved. Therefore, turbine predictions using numerical approaches remain challenge. This paper presents methodology that couples...

10.1016/j.renene.2024.120476 article EN cc-by Renewable Energy 2024-04-19

Jump penalty stabilization techniques for under-resolved turbulence have been recently proposed continuous and discontinuous high order Galerkin schemes [1], [2], [3]. The relies on the gradient or solution discontinuity at element interfaces to incorporate localised numerical diffusion in scheme. This acts as an implicit subgrid model stablizes turbulent simulations. paper investigates effect of jump methods (penalising solution) improvement high-order regime. We analyze these using...

10.1016/j.jcp.2023.112399 article EN cc-by-nc-nd Journal of Computational Physics 2023-07-28

This paper compares two actuator line methodologies for modelling wind turbines employing high-order h/p solvers and large-eddy simulations. The methods combine the accuracy of (in this work maximum order is 6) with computational efficiency lines to capture aerodynamic effects turbine blades. Comparisons experiments validate methodologies. We explore polynomial smoothing parameter associated Gaussian regularization function, use them blend forcing in mesh, show that both parameters influence...

10.48550/arxiv.2406.09993 preprint EN arXiv (Cornell University) 2024-06-14

We present the latest developments of our High-Order Spectral Element Solver (HORSES3D), an open source high-order discontinuous Galerkin framework, capable solving a variety flow applications, including compressible flows (with or without shocks), incompressible flows, various RANS and LES turbulence models, particle dynamics, multiphase aeroacoustics. provide overview spatial discretisation (including energy/entropy stable schemes) anisotropic p-adaptation capabilities. The solver is...

10.48550/arxiv.2206.09733 preprint EN other-oa arXiv (Cornell University) 2022-01-01

With the aim of minimising losses produced by fire accidents, engineering applies physics and principles to preserve integrity people, environment infrastructure. Fire modelling is complex due interaction between chemistry, heat transfer fluid dynamics. Commercially available simulation tools necessarily simplify this complexity, excluding less fundamental processes, such as soot production. By not including compound in simulations, interactions radiation transfer, propagation toxicity must...

10.1177/0734904120905579 article EN Journal of Fire Sciences 2020-03-01

View Video Presentation: https://doi.org/10.2514/6.2022-0413.vid We use a implicit Large Eddy Simulations methodology on under-resolved meshes to compute the aeroacoustic generated by Siemens-Gamesa airfoil. The solver employ high order discontiuous Galerkin spectral element scheme supplemented with stabilising split-form entropy-stable formulation. aim is compare direct computations of far field pressure fluctuations those obtained Ffowcs Williams and Hawkings predictions. Specifically, we...

10.2514/6.2022-0413 article EN AIAA SCITECH 2022 Forum 2022-01-03

We present a framework for airfoil shape optimization to reduce the trailing edge noise design of wind turbine blades. Far-field is evaluated using Amiet's theory coupled with TNO-Blake model calculate wall pressure spectrum and fast turn-around XFOIL simulations evaluate boundary layer parameters. The computational first validated NACA0012 at 0 angle attack. Particle swarm used find optimized configuration. multi-objective minimizes A-weighted overall sound level various angles attack,...

10.2139/ssrn.4236021 article EN SSRN Electronic Journal 2022-01-01

Aerodynamic noise is a limitation for further exploitation of wind energy resources. As this type caused by the interaction turbulent flow with airframe, detailed resolution necessary to obtain an accurate prediction far-field noise. Computational fluid dynamic (CFD) solvers simulate field but only at high computational cost, which much increased when acoustic resolved. Therefore, turbine predictions using numerical approaches remain challenge. This paper presents methodology that couples...

10.2139/ssrn.4723808 preprint EN 2024-01-01

This paper explores two Large Eddy Simulation (LES) approaches within the framework of high-order discontinuous Galerkin solver, Horses3D. The investigation focuses on an Inverted Multi-element Wing in Ground Effect (i.e. 2.5D Imperial Front section) representing a Formula 1 front wing, and compares strengths limitations LES methods. explicit formulation relies Vreman model, that adapts to laminar, transitional turbulent regimes. numerical uses nodal basis functions Gauss points. implicit...

10.48550/arxiv.2402.10913 preprint EN arXiv (Cornell University) 2024-01-15

We propose a reinforcement learning strategy to control wind turbine energy generation by actively changing the rotor speed, yaw angle and blade pitch angle. A double deep Q-learning with prioritized experience replay agent is coupled element momentum model trained allow for winds. The decide best (speed, yaw, pitch) simple steady winds subsequently challenged real dynamic turbulent winds, showing good performance. Q- compared classic value iteration both strategies outperform PID in all...

10.48550/arxiv.2402.11384 preprint EN arXiv (Cornell University) 2024-02-17

We present a novel approach to automate and optimize anisotropic p-adaptation in high-order h/p solvers using Reinforcement Learning (RL). The dynamic RL adaptation uses the evolving solution adjust polynomials. develop an offline training approach, decoupled from main solver, which shows minimal overcost when performing simulations. In addition, we derive RL-based error estimation that enables quantification of local discretization errors. proposed methodology is agnostic both computational...

10.48550/arxiv.2407.19000 preprint EN arXiv (Cornell University) 2024-07-26

High-order solvers are accurate but computationally expensive as they require small time steps to advance the solution in time. In this work, we include a corrective forcing low-order achieve high accuracy while advancing with larger and achieving fast computations. This work is continuation of our previous research [Manrique de Lara Ferrer, “Accelerating order discontinuous Galerkin using neural networks: 1D Burgers' equation,” Comput. Fluids 235, 105274 (2022) F. Manrique E. 3D...

10.1063/5.0225704 article EN Physics of Fluids 2024-10-01

We develop a torque-pitch control framework using deep reinforcement learning for wind turbines to optimize the generation of turbine energy while minimizing operational noise. employ double Q-learning, coupled blade element momentum solver, enable precise over parameters. In addition momentum, we use acoustic model Brooks Pope and Marcolini. Through training with simple winds, agent learns optimal policies that allow efficient complex turbulent winds. Our experiments demonstrate is able...

10.48550/arxiv.2407.13320 preprint EN arXiv (Cornell University) 2024-07-18

Jump penalty stabilisation techniques have been recently proposed for continuous and discontinuous high order Galerkin schemes [1,2,3]. The relies on the gradient or solution discontinuity at element interfaces to incorporate localised numerical diffusion in scheme. This acts as an implicit subgrid model stablises under-resolved turbulent simulations. paper investigates effect of jump methods (penalising solution) improvement high-order regime. We analyse these using eigensolution analysis,...

10.48550/arxiv.2208.11426 preprint EN cc-by arXiv (Cornell University) 2022-01-01

We present a framework for airfoil shape optimization to reduce the trailing edge noise design of wind turbine blades. Far-field is evaluated using Amiet's theory coupled with TNO-Blake model calculate wall pressure spectrum and fast turn-around XFOIL simulations evaluate boundary layer parameters. The computational first validated NACA0012 at zero angle attack. Particle swarm used find optimized configuration. multi-objective minimizes A-weighted overall sound level various angles attack,...

10.48550/arxiv.2210.00101 preprint EN other-oa arXiv (Cornell University) 2022-01-01

We propose a reinforcement learning strategy to control wind turbine energy generation, by actively changing the rotor speed, yaw angle and blade pitch angle. A double deep Q-Learning with prioritized experience replay agent is coupled element momentum model trained allow for winds. The decide best (speed, yaw, pitch) simple steady winds subsequently challenged real dynamic turbulent winds, showing good performance. shown outperform classic PID in all environments shows be well suited great...

10.2139/ssrn.4626683 preprint EN 2023-01-01
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