Sergio Avila-Sanchez

Dr. Sergio Avila-Sanchez

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Research Focus & Metrics

Academic Career Length

17Years (2010-Present)

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

Representative Publications

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1 July 2012 in Applied Mathematical Modelling
Verified
Journal Article
Closed access
ABAntonio Barrero-Gil
Antonio Barrero-Gil
SPSantiago Pindado
Santiago Pindado
SSergio Avila-Sanchez
Sergio Avila-Sanchez

1 November 2016 in Engineering Structures
Verified
Journal Article
Open access
SSergio Avila-Sanchez
Sergio Avila-Sanchez
OLO. Lopez-Garcia
O. Lopez-Garcia
ACA. Cuerva
A. Cuerva
JMJ. Meseguer
J. Meseguer

1 October 2017 in International Journal of Mechanical Sciences
Verified
Journal Article
Closed access
SSergio Avila-Sanchez
Sergio Avila-Sanchez
OLO. Lopez-Garcia
O. Lopez-Garcia
ACA. Cuerva
A. Cuerva
JMJ. Meseguer
J. Meseguer

10 May 2012 in Sensors
Verified
Journal Article
Open access
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SPSantiago Pindado
Santiago Pindado
JPJavier PEREZ-ALVAREZ
Javier PEREZ-ALVAREZ
SSergio Avila-Sanchez
Sergio Avila-Sanchez
The influence of anemometer rotor shape parameters, such as the cups’ front area or their center rotation radius on the anemometer’s performance was analyzed. This analysis was based on calibrations performed on two different anemometers (one based on magnet system output signal, and the other one based on an opto-electronic system output signal), tested with 21 different rotors. The results were compared to the ones resulting from classical analytical models. The results clearly showed a linear dependency of both calibration constants, the slope and the offset, on the cups’ center rotation radius, the influence of the front area of the cups also being observed. The analytical model of Kondo et al. was proved to be accurate if it is based on precise data related to the aerodynamic behavior of a rotor’s cup.

1 March 2014 in Journal of Wind Engineering and Industrial Aerodynamics
Verified
Journal Article
Open access
CDCian James Desmond
Cian James Desmond
SWSimon Watson
Simon Watson
SASandrine Aubrun
Sandrine Aubrun
SSergio Avila-Sanchez
Sergio Avila-Sanchez
PHPhilip Hancock
Philip Hancock
ASAdam Sayer
Adam Sayer
A series of numerical simulations of the flow over a forest stand have been conducted using two different turbulence closure models along with various levels of canopy morphology data. Simulations have been validated against Stereoscopic Particle Image Velocimetry measurements from a wind tunnel study using one hundred architectural model trees, the porosities of which have been assessed using a photographic technique.\ud It has been found that an accurate assessment of the porosity of the canopy, and specifically the variability with height, improves simulation quality regardless of the turbulence closure model used or the level of canopy geometry included. The observed flow field and recovery of the wake is in line with characteristic canopy flows published in the literature and it was found that the Shear Stress Transport turbulence model was best able to capture this detail numerically

1 February 2014 in Applied Energy
Verified
Journal Article
Open access
EGE. Torres García
E. Torres García
MOM. Ogueta-Gutiérrez
M. Ogueta-Gutiérrez
SSergio Avila-Sanchez
Sergio Avila-Sanchez
SFSebastián Franchini
Sebastián Franchini
EHE. Herrera
E. Herrera
JMJ. Meseguer
J. Meseguer
Parabolic reflectors, also known as parabolic troughs, are widely used in solar thermal power plants. This kind of power plants is usually located on desert climates, where the combined action of wind and dust can be of paramount importance. In some cases it becomes necessary to protect these devices from the joined wind and sand action, which is normally accomplished through solid windbreaks. In this paper the results of a wind tunnel test campaign, of a scale parabolic trough row having different windward windbreaks, are reported. The windbreaks herein considered consist of a solid wall with an upper porous fence. Different geometrical configurations, varying the solid wall height and the separation between the parabolic trough row and the windbreak have been considered. From the measured time series, both the mean and peak values of the aerodynamic loads were determined. As it would be expected, mean aerodynamic drag, as well as peak values, decrease as the distance between the windbreak and the parabolic increases, and after a threshold value, such drag loads increase with the distance