José Francisco Herbert Acero

Mr. José Francisco Herbert Acero


Research Focus & Metrics

Academic Career Length

13Years (2014-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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29 October 2014 in Energies
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Journal Article
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JAJosé Francisco Herbert Acero
José Francisco Herbert Acero
OPOliver Probst
Oliver Probst
PRPierre-Elouan Réthoré
Pierre-Elouan Réthoré
GLGunner Larsen
Gunner Larsen
KCKrystel Castillo-Villar
Krystel Castillo-Villar
This article presents a review of the state of the art of the Wind Farm Design and Optimization (WFDO) problem. The WFDO problem refers to a set of advanced planning actions needed to extremize the performance of wind farms, which may be composed of a few individual Wind Turbines (WTs) up to thousands of WTs. The WFDO problem has been investigated in different scenarios, with substantial differences in main objectives, modelling assumptions, constraints, and numerical solution methods. The aim of this paper is: (1) to present an exhaustive survey of the literature covering the full span of the subject, an analysis of the state-of-the-art models describing the performance of wind farms as well as its extensions, and the numerical approaches used to solve the problem; (2) to provide an overview of the available knowledge and recent progress in the application of such strategies to real onshore and offshore wind farms; and (3) to propose a comprehensive agenda for future research.

1 January 2015 in Mathematical Problems in Engineering
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Journal Article
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JAJosé Francisco Herbert Acero
José Francisco Herbert Acero
OPOliver Probst
Oliver Probst
Carlos Rivera-SolorioCarlos Rivera-Solorio
Carlos Rivera-Solorio
KCKrystel K. Castillo-Villar
Krystel K. Castillo-Villar
SMSantos Méndez-Díaz
Santos Méndez-Díaz
This work presents the analysis, application, and comparison of thirteen fluid flow models in the prediction of two-dimensional airfoil aerodynamics, considering laminar and turbulent subsonic inflow conditions. Diverse sensitivity analyses of different free parameters (e.g., the domain topology and its discretization, the flow model, and the solution method together with its convergence mechanisms) revealed important effects on the simulations’ outcomes. The NACA 4412 airfoil was considered throughout the work and the computational predictions were compared with experiments conducted under a wide range of Reynolds numbers (7e5≤Re≤9e6) and angles-of-attack (-10°≤α≤20°). Improvements both in modeling accuracy and processing time were achieved by considering the RS LP-S and the Transition SST turbulence models, and by considering finite volume-based solution methods with preconditioned systems, respectively. The RS LP-S model provided the best lift force predictions due to the adequate modeling of the micro and macro anisotropic turbulence at the airfoil’s surface and at the nearby flow field, which in turn allowed the adequate prediction of stall conditions. The Transition-SST model provided the best drag force predictions due to adequate modeling of the laminar-to-turbulent flow transition and the surface shear stresses. Conclusions, recommendations, and a comprehensive research agenda are presented based on validated computational results.

1 January 2014 in Mathematical Problems in Engineering
Verified
Journal Article
Open access
PDF file
JAJosé Francisco Herbert Acero
José Francisco Herbert Acero
JMJaime Martínez-Lauranchet
Jaime Martínez-Lauranchet
OPOliver Probst
Oliver Probst
SMSantos Méndez-Díaz
Santos Méndez-Díaz
KCKrystel K. Castillo-Villar
Krystel K. Castillo-Villar
PRPierre-Elouan Réthoré
Pierre-Elouan Réthoré
This work presents a novel framework for the aerodynamic design and optimization of blades for small horizontal axis wind turbines (WT). The framework is based on a state‐of‐the‐art blade element momentum model, which is complemented with the XFOIL 6.96 software in order to provide an estimate of the sectional blade aerodynamics. The framework considers an innovative nested‐hybrid solution procedure based on two metaheuristics, the virtual gene genetic algorithm and the simulated annealing algorithm, to provide a near‐optimal solution to the problem. The objective of the study is to maximize the aerodynamic efficiency of small WT (SWT) rotors for a wide range of operational conditions. The design variables are (1) the airfoil shape at the different blade span positions and the radial variation of the geometrical variables of (2) chord length, (3) twist angle, and (4) thickness along the blade span. A wind tunnel validation study of optimized rotors based on the NACA 4‐digit airfoil series is presented. Based on the experimental data, improvements in terms of the aerodynamic efficiency, the cut‐in wind speed, and the amount of material used during the manufacturing process were achieved. Recommendations for the aerodynamic design of SWT rotors are provided based on field experience.