Andrea Ianiro
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Andrea Ianiro has a total of 106 co-authors. Here are the top co-authors by number of shared publications:
- Stefano Discetti
Universidad Carlos III de Madrid
46 shared publications - Gennaro Cardone
University of Naples “Federico II”, 80125 Naples, Italy
15 shared publications - Marco Raiola
Universidad Carlos III de Madrid
12 shared publications - Ricardo Vinuesa
University of Michigan
8 shared publications - Iacopo Tirelli
Universidad Carlos III de Madrid
7 shared publications - Rodrigo Castellanos
Universidad Carlos III de Madrid
7 shared publications
Latest Publications
- Open Access
- 25 August 2026
- Published by IOP Publishing in Measurement Science and Technology
- Vol. 37 (34) , 341001
Event-based sensing for turbulent flows: a measurement science perspective on information-efficient estimation and control
Event-based sensing offers a promising alternative to conventional frame-based measurement in turbulent flows, where intermittency, multiscale dynamics, and stringent latency constraints can make dense uniform sampling both expensive and redundant. Rather than acquiring less data, the goal is to acquire more-relevant data: measurements triggered by dynamically meaningful changes that reduce uncertainty in control-relevant flow coordinates. We leverage ideas from reduced-order modeling, sparse observability, biological mechanosensors, and event-based signal processing to outline a conceptual framework in which turbulent flows are sensed through asynchronous measurements, encoded at the hardware level, and processed by hybrid observers or neuromorphic architectures. A simple analytical argument shows that the estimation-error advantage of event-based encoding over uniform sampling scales directly with the temporal intermittency of the observable. Experimental demonstrations remain limited but encouraging. This perspective reframes the sensing bottleneck in turbulence as a problem of information relevance rather than sample count, and sets out a research agenda covering reduced-state targets, trigger policies, asynchronous observers, uncertainty quantification, and reproducible benchmarking.
- 25 August 2026
- Published by IOP Publishing in Measurement Science and Technology
- Vol. 37 (34) , 341001
Open AccessEvent-based sensing for turbulent flows: a measurement science perspective on information-efficient estimation and control
Event-based sensing offers a promising alternative to conventional frame-based measurement in turbulent flows, where intermittency, multiscale dynamics, and stringent latency constraints can make dense uniform sampling both expensive and redundant. Rather than acquiring less data, the goal is to acquire more-relevant data: measurements triggered by dynamically meaningful changes that reduce uncertainty in control-relevant flow coordinates. We leverage ideas from reduced-order modeling, sparse observability, biological mechanosensors, and event-based signal processing to outline a conceptual framework in which turbulent flows are sensed through asynchronous measurements, encoded at the hardware level, and processed by hybrid observers or neuromorphic architectures. A simple analytical argument shows that the estimation-error advantage of event-based encoding over uniform sampling scales directly with the temporal intermittency of the observable. Experimental demonstrations remain limited but encouraging. This perspective reframes the sensing bottleneck in turbulence as a problem of information relevance rather than sample count, and sets out a research agenda covering reduced-state targets, trigger policies, asynchronous observers, uncertainty quantification, and reproducible benchmarking.
- Open Access
- 3 July 2026
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 39 (11)
Information decomposition for disentangled and interpretable manifold learning of fluid flows via variational autoencoders
- 3 July 2026
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 39 (11)
Open AccessInformation decomposition for disentangled and interpretable manifold learning of fluid flows via variational autoencoders
- Open Access
- 20 June 2026
- Published by Elsevier in Experimental Thermal and Fluid Science
- Vol. 177
On the turbulent wake of the actuated fluidic pinball: Dynamics, bifurcations and control authority
- 20 June 2026
- Published by Elsevier in Experimental Thermal and Fluid Science
- Vol. 177
Open AccessOn the turbulent wake of the actuated fluidic pinball: Dynamics, bifurcations and control authority
- 1 June 2026
- Published by AIP Publishing in Physics of Fluids
- Vol. 38 (6)
Drag reduction via separation control using plasma actuators on a truck cabin side
We investigate the drag reduction on a heavy-duty vehicle using dielectric-barrier discharge plasma actuators located on the A-pillars. An experimental campaign is carried out on a generalized truck model, the Ground Transportation System (GTS), which is known for its lateral separation bubbles on both sides of the truck's cabin. Measurements are performed for several yaw angles up to 7.5°. Actuation is applied individually on the leeward and windward sides as well as simultaneously. Load cell measurements show that the plasma actuators effectively reduce the axial force on the GTS, with symmetric actuation achieving the highest reduction. Leeward actuation demonstrates greater control authority than the windward one; at large yaw angles the latter has a negligible effect on the axial force. Regarding side force, the leeward actuation produces a drop in its magnitude while windward actuation produces an increase. Interestingly, actuating symmetrically also augments the side force. Particle image velocimetry reveals that the plasma actuator causes a reduction in the length and width of the separation bubble on the cabin side, reducing the apparent frontal area of the truck and thus its drag. Under crosswind conditions, the stronger authority of the leeward actuator is explained by the larger separation bubble. The side force variation is driven by the net lateral suction force, which correlates with the size of the lateral recirculation regions controlled by the actuators.
- 1 June 2026
- Published by AIP Publishing in Physics of Fluids
- Vol. 38 (6)
Drag reduction via separation control using plasma actuators on a truck cabin side
We investigate the drag reduction on a heavy-duty vehicle using dielectric-barrier discharge plasma actuators located on the A-pillars. An experimental campaign is carried out on a generalized truck model, the Ground Transportation System (GTS), which is known for its lateral separation bubbles on both sides of the truck's cabin. Measurements are performed for several yaw angles up to 7.5°. Actuation is applied individually on the leeward and windward sides as well as simultaneously. Load cell measurements show that the plasma actuators effectively reduce the axial force on the GTS, with symmetric actuation achieving the highest reduction. Leeward actuation demonstrates greater control authority than the windward one; at large yaw angles the latter has a negligible effect on the axial force. Regarding side force, the leeward actuation produces a drop in its magnitude while windward actuation produces an increase. Interestingly, actuating symmetrically also augments the side force. Particle image velocimetry reveals that the plasma actuator causes a reduction in the length and width of the separation bubble on the cabin side, reducing the apparent frontal area of the truck and thus its drag. Under crosswind conditions, the stronger authority of the leeward actuator is explained by the larger separation bubble. The side force variation is driven by the net lateral suction force, which correlates with the size of the lateral recirculation regions controlled by the actuators.
- 1 April 2026
- Published by AIP Publishing in Physics of Fluids
- Vol. 38 (4)
Sensor optimization for urban wind estimation with a cluster-based probabilistic framework
We propose a physics-informed machine-learned framework for sensor-based flow estimation for drone trajectories in complex urban terrain. The input is a rich set of flow simulations at many wind conditions. The outputs are velocity and uncertainty estimates for a target domain and subsequent sensor optimization for minimal uncertainty. The framework has three innovations compared to traditional flow estimators. First, the algorithm scales proportionally to the domain complexity, making it suitable for flows that are too complex for any monolithic reduced-order representation. Second, the framework extrapolates beyond the training data, e.g., smaller and larger wind velocities. Last and perhaps most importantly, the sensor location is a free input, significantly extending the vast majority of the literature. The key enablers are (1) a Reynolds number-based scaling of the flow variables, (2) a physics-based domain decomposition, (3) a cluster-based flow representation for each subdomain, (4) an information entropy correlating the subdomains, and (5) a multi-variate probability function relating sensor input and targeted velocity estimates. This framework is demonstrated using drone flight paths through a three-building cluster as a simple example. We anticipate adaptations and applications for estimating complete cities and incorporating weather input.
- 1 April 2026
- Published by AIP Publishing in Physics of Fluids
- Vol. 38 (4)
Sensor optimization for urban wind estimation with a cluster-based probabilistic framework
We propose a physics-informed machine-learned framework for sensor-based flow estimation for drone trajectories in complex urban terrain. The input is a rich set of flow simulations at many wind conditions. The outputs are velocity and uncertainty estimates for a target domain and subsequent sensor optimization for minimal uncertainty. The framework has three innovations compared to traditional flow estimators. First, the algorithm scales proportionally to the domain complexity, making it suitable for flows that are too complex for any monolithic reduced-order representation. Second, the framework extrapolates beyond the training data, e.g., smaller and larger wind velocities. Last and perhaps most importantly, the sensor location is a free input, significantly extending the vast majority of the literature. The key enablers are (1) a Reynolds number-based scaling of the flow variables, (2) a physics-based domain decomposition, (3) a cluster-based flow representation for each subdomain, (4) an information entropy correlating the subdomains, and (5) a multi-variate probability function relating sensor input and targeted velocity estimates. This framework is demonstrated using drone flight paths through a three-building cluster as a simple example. We anticipate adaptations and applications for estimating complete cities and incorporating weather input.
- 12 February 2026
- Published by American Physical Society (APS) in Physical Review Fluids
- Vol. 11 (2)
Meshless super-resolution of scattered data via constrained radial basis functions and K-nearest-neighbors-driven densification
- 12 February 2026
- Published by American Physical Society (APS) in Physical Review Fluids
- Vol. 11 (2)
Meshless super-resolution of scattered data via constrained radial basis functions and K-nearest-neighbors-driven densification
- Open Access
- 30 January 2026
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 1028
Assessment of non-intrusive sensing in wall-bounded turbulence through explainable deep learning
In this work we present a framework to explain the prediction of the velocity fluctuation at a certain wall-normal distance from wall measurements with a deep-learning model. For this purpose, we apply the deep-SHAP (deep Shapley additive explanations) method to explain the velocity fluctuation prediction in wall-parallel planes in a turbulent open channel at a friction Reynolds number ${\textit{Re}}_\tau =180$ . The explainable-deep-learning methodology comprises two stages. The first stage consists of training the estimator. In this case, the velocity fluctuation at a wall-normal distance of 15 wall units is predicted from the wall-shear stress and wall-pressure. In the second stage, the deep-SHAP algorithm is applied to estimate the impact each single grid point has on the output. This analysis calculates an importance field, and then, correlates the high-importance regions calculated through the deep-SHAP algorithm with the wall-pressure and wall-shear stress distributions. The grid points are then clustered to define structures according to their importance. We find that the high-importance clusters exhibit large pressure and shear-stress fluctuations, although generally not corresponding to the highest intensities in the input datasets. Their typical values averaged among these clusters are equal to one to two times their standard deviation and are associated with streak-like regions. These high-importance clusters present a size between 20 and 120 wall units, corresponding to approximately 100 and 600 $\unicode{x03BC} \textrm {m}$ for the case of a commercial aircraft.- 30 January 2026
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 1028
Open AccessAssessment of non-intrusive sensing in wall-bounded turbulence through explainable deep learning
In this work we present a framework to explain the prediction of the velocity fluctuation at a certain wall-normal distance from wall measurements with a deep-learning model. For this purpose, we apply the deep-SHAP (deep Shapley additive explanations) method to explain the velocity fluctuation prediction in wall-parallel planes in a turbulent open channel at a friction Reynolds number ${\textit{Re}}_\tau =180$ . The explainable-deep-learning methodology comprises two stages. The first stage consists of training the estimator. In this case, the velocity fluctuation at a wall-normal distance of 15 wall units is predicted from the wall-shear stress and wall-pressure. In the second stage, the deep-SHAP algorithm is applied to estimate the impact each single grid point has on the output. This analysis calculates an importance field, and then, correlates the high-importance regions calculated through the deep-SHAP algorithm with the wall-pressure and wall-shear stress distributions. The grid points are then clustered to define structures according to their importance. We find that the high-importance clusters exhibit large pressure and shear-stress fluctuations, although generally not corresponding to the highest intensities in the input datasets. Their typical values averaged among these clusters are equal to one to two times their standard deviation and are associated with streak-like regions. These high-importance clusters present a size between 20 and 120 wall units, corresponding to approximately 100 and 600 $\unicode{x03BC} \textrm {m}$ for the case of a commercial aircraft. - 17 September 2025
- Published by American Physical Society (APS) in Physical Review Fluids
- Vol. 10 (9)
Resolving convective velocities of turbulent boundary layer-induced convective heat transfer fluctuations at the wall
- 17 September 2025
- Published by American Physical Society (APS) in Physical Review Fluids
- Vol. 10 (9)
Resolving convective velocities of turbulent boundary layer-induced convective heat transfer fluctuations at the wall
- 3 June 2025
- Published by American Physical Society (APS) in Physical Review Fluids
- Vol. 10 (8)
Model-based time super-sampling of turbulent flow field sequences
- 3 June 2025
- Published by American Physical Society (APS) in Physical Review Fluids
- Vol. 10 (8)
Model-based time super-sampling of turbulent flow field sequences
- Open Access
- 13 May 2025
- Published by Springer Nature in Experiments in Fluids
- Vol. 66 (6) , 1-17
Full-domain POD modes from PIV asynchronous patches
A method is proposed to obtain full-domain spatial modes based on proper orthogonal decomposition (POD) of particle image velocimetry (PIV) measurements taken at different (overlapping) spatial locations. This situation occurs when large domains are covered by multiple non-simultaneous measurements and yet the large-scale flow field organization is to be captured. The proposed methodology leverages the definition of POD spatial modes as eigenvectors of the spatial correlation matrix, where local measurements, even when not obtained simultaneously, provide each a portion of the latter, which is then analyzed to synthesize the full-domain spatial modes. The measurement domain coverage is found to require regions overlapping by 50–75% to yield a smooth distribution of the modes. The procedure identifies structures twice as large as each measurement patch. The technique, referred to as Patch POD, is applied to planar PIV data of a submerged jet flow where the effect of patching is simulated by splitting the original PIV data. Patch POD is then extended to 3D robotic measurement around a wall-mounted cube. The results show that the patching technique enables global modal analysis over a domain covered with a multitude of non-simultaneous measurements.
- 13 May 2025
- Published by Springer Nature in Experiments in Fluids
- Vol. 66 (6) , 1-17
Open AccessFull-domain POD modes from PIV asynchronous patches
A method is proposed to obtain full-domain spatial modes based on proper orthogonal decomposition (POD) of particle image velocimetry (PIV) measurements taken at different (overlapping) spatial locations. This situation occurs when large domains are covered by multiple non-simultaneous measurements and yet the large-scale flow field organization is to be captured. The proposed methodology leverages the definition of POD spatial modes as eigenvectors of the spatial correlation matrix, where local measurements, even when not obtained simultaneously, provide each a portion of the latter, which is then analyzed to synthesize the full-domain spatial modes. The measurement domain coverage is found to require regions overlapping by 50–75% to yield a smooth distribution of the modes. The procedure identifies structures twice as large as each measurement patch. The technique, referred to as Patch POD, is applied to planar PIV data of a submerged jet flow where the effect of patching is simulated by splitting the original PIV data. Patch POD is then extended to 3D robotic measurement around a wall-mounted cube. The results show that the patching technique enables global modal analysis over a domain covered with a multitude of non-simultaneous measurements.