Marco Raiola

ORCID: 0000-0003-2744-6347
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About
Contact & Profiles
Research Areas
  • Fluid Dynamics and Turbulent Flows
  • Aerodynamics and Acoustics in Jet Flows
  • Model Reduction and Neural Networks
  • Wind and Air Flow Studies
  • Fluid Dynamics and Vibration Analysis
  • Biomimetic flight and propulsion mechanisms
  • Heat Transfer Mechanisms
  • Flow Measurement and Analysis
  • Hydraulic and Pneumatic Systems
  • Combustion and flame dynamics
  • Nuclear Engineering Thermal-Hydraulics
  • Plasma and Flow Control in Aerodynamics
  • Fault Detection and Control Systems
  • Probabilistic and Robust Engineering Design
  • Aerodynamics and Fluid Dynamics Research
  • Particle Dynamics in Fluid Flows
  • Computational Fluid Dynamics and Aerodynamics
  • Micro and Nano Robotics
  • Robotic Path Planning Algorithms
  • Cavitation Phenomena in Pumps
  • Advanced Image Processing Techniques
  • Image and Signal Denoising Methods
  • Wind Energy Research and Development
  • Seismic Imaging and Inversion Techniques

Universidad Carlos III de Madrid
2015-2024

University of Waterloo
2018

Delft University of Technology
2018

10.1016/j.expthermflusci.2025.111407 article EN cc-by Experimental Thermal and Fluid Science 2025-01-01

A novel method to improve the accuracy of pressure field estimation from time-resolved Particle Image Velocimetry data is proposed. This generates several new time-series velocity by propagating in time original one using an advection-based model, which assumes that small-scale turbulence advected large-scale motions. Then smoothing performed at corresponding positions across all generated time-series. The process repeated through iterative scheme. proposed technique smears out spatial noise...

10.48550/arxiv.2501.06060 preprint EN arXiv (Cornell University) 2025-01-10

10.1016/j.expthermflusci.2025.111448 article EN Experimental Thermal and Fluid Science 2025-03-01

The most explored path to obtain pressure fields from Particle Image Velocimetry (PIV) data roots its basis on accurate measurement of instantaneous velocity and their corresponding time derivatives. This requires time-resolved measurements, which are often difficult achieve due hardware limitations expensive implement. In alternative, snapshot PIV experiments more affordable but require enforcing physical constraints (e.g. Taylor's hypothesis) extract the derivative field. this work, we...

10.1016/j.expthermflusci.2022.110647 article EN cc-by Experimental Thermal and Fluid Science 2022-04-19

This study focuses on an active strategy for unsteady-load control by means of a trailing-edge flap. Experiments 2D pitching and heaving NACA 0018 airfoil with actuated flap are performed at reduced frequency in free-stream flow . The model is equipped 24 differential pressure transducers to provide the time-resolved distribution difference between suction sides. Results show that significantly decreases magnitude unsteady loads. A order effect loads proposed. estimated adding contribution...

10.2514/1.j056342 article EN AIAA Journal 2018-01-02

10.1016/j.expthermflusci.2016.06.003 article EN Experimental Thermal and Fluid Science 2016-06-11

Abstract This work presents an experimental setup for acquiring synchronized wall and flow field measurements in a turbulent boundary layer (TBL). Instantaneous of the convective heat transfer distribution at are carried out simultaneously, using wall-parallel planar particle image velocimetry infrared thermography. A low-thermal-inertia heated-thin-foil sensor is embedded beneath TBL to measure temperature maps with enough temporal resolution. The unsteady energy balance heated foil can be...

10.1088/1361-6501/ace8ad article EN Measurement Science and Technology 2023-08-10

"This study investigates the feasibility of using neuromorphic event-based vision (EBV) camera for low-order modelling, a key enabler real-time flow control. A synchronized experiment with simultaneous Event Based Image Velocimetry (EBIV) and Particle (PIV) is performed on submerged water jet at Re = 2600. Flow statistics, spectral content, reduced-order modeling capabilities Proper Orthogonal Decomposition (POD) are assessed. Velocity fields computed via standard PIV processing compared...

10.55037/lxlaser.21st.222 article EN 2024-07-08

The convective heat transfer enhancement in a turbulent boundary layer (TBL) employing pulsed, slot jet crossflow is investigated experimentally. A parametric study on actuation frequencies and duty cycles performed. actuator flush-mounted that injects fluid into well-behaved zero-pressure-gradient TBL over flat plate. heated-thin-foil sensor measures the time-averaged coefficient downstream of location flow field characterised by means Particle Image Velocimetry. results show both...

10.1016/j.applthermaleng.2022.119595 article EN cc-by-nc-nd Applied Thermal Engineering 2022-11-05

Ensemble Particle Tracking Velocimetry (EPTV) is a method to extract high-resolution statistical information on flow fields from Image (PIV) images. The process based tracking particles and extracting the velocity probability distribution functions of image ensemble in averaging-regions deemed contain sufficient number of particle pairs/tracks. The size averaging regions depends particle density the number snapshots. An automatic adaptive variation PTV presented to further push spatial...

10.1088/1361-6501/ab82bf article EN Measurement Science and Technology 2020-05-27

This paper reports a combined experimental and numerical study of the flow over rigid airfoil in flapping motion. The setup consists heaving pitching at moderate Reynolds number ([Formula: see text]), Strouhal St = 0.1. aim is to assess accuracy two-dimensional direct simulations predicting aerodynamic forces configuration, which nominally but verge three-dimensionality. assessment carried out with experiments, including field force measurements particle image velocimetry load cell....

10.1177/0954410019867570 article EN Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2019-08-19

10.1016/j.expthermflusci.2020.110234 article EN Experimental Thermal and Fluid Science 2020-09-04

This paper reports a comparison between wind-tunnel measurements and numerical simulations to assess the capabilities of Reynolds-Averaged Navier-Stokes models estimate wind load over solar-panel arrays. The free airstream impinging on arrays creates complex separated flow at large Reynolds number, which is severely challenging for current models. compared in this article are k-ϵ, Shear-Stress Transport k-ω, transition Shear Model. Particle Image Velocimetry performed investigate mean...

10.3390/app11062496 article EN cc-by Applied Sciences 2021-03-11

This paper discusses the integration of an air collector and dissipation cavity into a closed anechoic chamber for jet noise studies. Having issued directly in introduces recirculation effects, which influence plume, producing different flow compared to free emitted open environment. The implementation aims redirect, dissipate extract effectively airflow downstream region chamber. fact being closed-section facility provokes recirculation, influences potential core plume. However, any...

10.2514/6.2024-3066 article EN 28th AIAA/CEAS Aeroacoustics 2022 Conference 2024-05-30
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