A. Grille Guerra
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13 records found
1
The scalability of experiments using PIV relies upon several parameters: primarily the tracers scattering cross section and their concentration, the power and distribution of illumination; and the imagers sensor size and their amount. Given their larger cross section, helium-filled soap bubbles (HFSB) allow measurements in air flows over a significantly larger domain compared to traditional oil or water droplets. Controlling their diameter translates into scalability of the experiment. In chapter 3, a technique is presented to extend the control of HFSB diameter by geometrical variations of the generator. A theoretical model predicts the bubble size and production rate, which is verified experimentally by high-speed shadow visualization. The overall range of HFSB produced in a stable regime can be varied from approximately 150 μm, targeting experiments in research facilities at high spatial resolution, to a few millimetres, sufficient for large-scale measurements in industrial facilities as well as full-scale on-site experiments. Imaging by light scattering of such tracers is also investigated, in view of controversies in the literature on whether diffraction or geometrical imaging dominate the imaging regime. For large-scale volumetric applications, it is shown that varying the bubble diameter allows increasing both the measurement domain as well as the working distance of the imagers at 10 m and beyond.
Measuring the velocity field around a complex object by volumetric PIV is hindered by shadow formation (illumination), camera occlusion (imaging) and light reflections from the object surface. The former have been recently dealt with by multiplying illumination and imaging directions (redundancy) and by the integration of ray-tracing techniques to include the effect of visual blockage caused by the object. Instead, the problem of light reflections blinding regions of the images has not been afforded yet. The latter pertains to interactions between illumination and imaging through the object surface and it poses additional challenges to ghost particle formation, particle detection and tracking in general, increasing the computational cost and reducing the accuracy of the measured velocity field. In chapter 4, a method is proposed to effectively detect such regions, and measures to modify the particle triangulation algorithm are devised. The viability of this novel approach is examined by application to two experiments of increasing complexity. The first case is the flow around a stationary wall-mounted cube as imaged with a redundant number of cameras. The second experiment tackles an elite runner sprinting across the measurement region obtained with the Ring-of-Fire technique. A considerable reduction of ghost particles (false positives) is attained, while the formation of voids (false negatives) is also minimized. The overall result of the method maximizes the measurement region around and in proximity of the object of interest.
Multiple-exposure (ME) recording is a variant of PIV whereby more than two samples of the particle position are obtained to overcome some limitations of single-exposure dual-frame recordings, such as accelerometry, pressure from instantaneous PIV data, or to further extend the dynamic velocity range. Compared to time-resolved systems, ME lowers system requirements in terms of laser power and camera frame rate, thus making it more suitable for applications involving a redundant number of cameras and higher flow velocities. In chapter 5, the reliability and accuracy of volumetric particle tracking in ME recordings comprising up to 5 exposures with one or two frames is first scrutinized on a synthetic particle field motion based on a Taylor-Green vortex lattice, yielding viable results. The measurement accuracy in terms of dynamic velocity and acceleration ranges is reported, as a function of particle image density, number of pulses and timing sequence. Besides, ME recordings are simulated from a time-resolved experiment around a wall-mounted cube, which yield equivalence between ME and time-resolved conditions. A demonstration of volumetric ME for accelerometry and pressure from PIV is also included, with experiments in the turbulent wake of a circular cylinder.
Modal decomposition of PIV measurements is a common approach to reduce data complexity and aid interpretability. In chapter 6, a method to reconstruct the dense velocity field from relatively sparse particle tracks, as obtained for instance from volumetric ME recordings, is introduced. The goal is to provide a representation of the 3D flow field on a Cartesian grid, for inspection of derived flow quantities, at high spatial resolution. The approach leverages the properties of proper orthogonal decomposition (POD) and it iteratively reconstructs the detailed spatial modes from a first, coarse estimation thereof. The initially coarse Cartesian representation of the velocity field is obtained by local data averaging, where POD is applied. The spatial resolution of the POD modes is enhanced by reprojecting them onto the sparse particles velocity to iteratively improve the reconstruction of the temporal coefficients. Finally, the enhanced velocity field is represented at high-resolution with a reduced order model using the dominant POD modes. Experiments in the wake of a cylinder at Re_D = 27,000 are used to assess the suitability of the method to resolve the turbulent Kármán-Benard wake. The approach is benchmarked against traditional as well as state-of-the-art reconstruction methods, illustrating the capability of enhancing the spatial resolution of sparse velocity data. ...
The scalability of experiments using PIV relies upon several parameters: primarily the tracers scattering cross section and their concentration, the power and distribution of illumination; and the imagers sensor size and their amount. Given their larger cross section, helium-filled soap bubbles (HFSB) allow measurements in air flows over a significantly larger domain compared to traditional oil or water droplets. Controlling their diameter translates into scalability of the experiment. In chapter 3, a technique is presented to extend the control of HFSB diameter by geometrical variations of the generator. A theoretical model predicts the bubble size and production rate, which is verified experimentally by high-speed shadow visualization. The overall range of HFSB produced in a stable regime can be varied from approximately 150 μm, targeting experiments in research facilities at high spatial resolution, to a few millimetres, sufficient for large-scale measurements in industrial facilities as well as full-scale on-site experiments. Imaging by light scattering of such tracers is also investigated, in view of controversies in the literature on whether diffraction or geometrical imaging dominate the imaging regime. For large-scale volumetric applications, it is shown that varying the bubble diameter allows increasing both the measurement domain as well as the working distance of the imagers at 10 m and beyond.
Measuring the velocity field around a complex object by volumetric PIV is hindered by shadow formation (illumination), camera occlusion (imaging) and light reflections from the object surface. The former have been recently dealt with by multiplying illumination and imaging directions (redundancy) and by the integration of ray-tracing techniques to include the effect of visual blockage caused by the object. Instead, the problem of light reflections blinding regions of the images has not been afforded yet. The latter pertains to interactions between illumination and imaging through the object surface and it poses additional challenges to ghost particle formation, particle detection and tracking in general, increasing the computational cost and reducing the accuracy of the measured velocity field. In chapter 4, a method is proposed to effectively detect such regions, and measures to modify the particle triangulation algorithm are devised. The viability of this novel approach is examined by application to two experiments of increasing complexity. The first case is the flow around a stationary wall-mounted cube as imaged with a redundant number of cameras. The second experiment tackles an elite runner sprinting across the measurement region obtained with the Ring-of-Fire technique. A considerable reduction of ghost particles (false positives) is attained, while the formation of voids (false negatives) is also minimized. The overall result of the method maximizes the measurement region around and in proximity of the object of interest.
Multiple-exposure (ME) recording is a variant of PIV whereby more than two samples of the particle position are obtained to overcome some limitations of single-exposure dual-frame recordings, such as accelerometry, pressure from instantaneous PIV data, or to further extend the dynamic velocity range. Compared to time-resolved systems, ME lowers system requirements in terms of laser power and camera frame rate, thus making it more suitable for applications involving a redundant number of cameras and higher flow velocities. In chapter 5, the reliability and accuracy of volumetric particle tracking in ME recordings comprising up to 5 exposures with one or two frames is first scrutinized on a synthetic particle field motion based on a Taylor-Green vortex lattice, yielding viable results. The measurement accuracy in terms of dynamic velocity and acceleration ranges is reported, as a function of particle image density, number of pulses and timing sequence. Besides, ME recordings are simulated from a time-resolved experiment around a wall-mounted cube, which yield equivalence between ME and time-resolved conditions. A demonstration of volumetric ME for accelerometry and pressure from PIV is also included, with experiments in the turbulent wake of a circular cylinder.
Modal decomposition of PIV measurements is a common approach to reduce data complexity and aid interpretability. In chapter 6, a method to reconstruct the dense velocity field from relatively sparse particle tracks, as obtained for instance from volumetric ME recordings, is introduced. The goal is to provide a representation of the 3D flow field on a Cartesian grid, for inspection of derived flow quantities, at high spatial resolution. The approach leverages the properties of proper orthogonal decomposition (POD) and it iteratively reconstructs the detailed spatial modes from a first, coarse estimation thereof. The initially coarse Cartesian representation of the velocity field is obtained by local data averaging, where POD is applied. The spatial resolution of the POD modes is enhanced by reprojecting them onto the sparse particles velocity to iteratively improve the reconstruction of the temporal coefficients. Finally, the enhanced velocity field is represented at high-resolution with a reduced order model using the dominant POD modes. Experiments in the wake of a cylinder at Re_D = 27,000 are used to assess the suitability of the method to resolve the turbulent Kármán-Benard wake. The approach is benchmarked against traditional as well as state-of-the-art reconstruction methods, illustrating the capability of enhancing the spatial resolution of sparse velocity data.
Recording onto a single-frame multiple exposures of the tracer particles has the potential to simplify the hardware needed for 3D PTV measurements, especially when dealing with high-speed flows. The analysis of such recordings, however, is challenged by the unknown time tag of each particle exposure, alongside their unknown organization into physical trajectories (trajectory tag). Using a sequence of two or more illumination pulses with a constant time separation leads to the well-known directional ambiguity problem, whereby it is not possible to distinguish the direction of motion of the tracer particles. Instead, an irregular and asymmetric sequence of time separation for the illumination pulses allows recognizing the time tag of the unique sequence of positions in the image, composing the trace. A criterion is formulated here that recognizes unambiguously the trace pattern, based upon the principle of kinematic similarity. A combinatorial algorithm is proposed whereby a signal-to-noise ratio is introduced for every candidate trace. The approach is combined with an additional criterion that favors trace regularity (minimum velocity fluctuations). The algorithm is illustrated making use of particle motion examples. Furthermore, it is assessed using 3D experimental data produced with time-resolved analysis (single-frame, single-exposure) using the Shake-the-Box method. Traces with a three-pulse sequence yield a detection rate of 85%. The latter declines with the number of pulses. Conversely, the error rate rapidly vanishes with the samples number, which confirms the reliability of trace detection criterion when more pulses are comprised in the sequence.
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.
The effects of the wing skin distortion on the boundary layer of a highly flexible wing are analyzed in a wind tunnel experiment using infrared thermography measurements. Considerable differences in the boundary layer flow are observed when comparing the sections of the wing near the ribs, where the design shape of the wing is preserved, and in between the ribs. At the spanwise locations between the ribs, the sectional wing shape distorts and triggers boundary layer transition close to the leading edge. The differences between the design behavior of the wing and the experimental results of the boundary layer analysis demonstrate the need for considering the skin deformation and its effects on the boundary layer flow when designing highly flexible wings.
A method to reconstruct the dense velocity field from relatively sparse particle tracks is introduced. The approach leverages the properties of proper orthogonal decomposition (POD), and it iteratively reconstructs the detailed spatial modes from a first, coarse estimation thereof. The initially coarse Cartesian representation of the velocity field is obtained by local data averaging, where POD is applied. The spatial resolution of the POD modes is enhanced by reprojecting them onto the sparse particle velocity to iteratively improve the reconstruction of the temporal coefficients. Finally, the enhanced velocity field is represented at high-resolution with a reduced order model using the dominant POD modes. The method is referred to as iterative modal reconstruction (IMR), as an extension of the recently proposed data-enhanced particle tracking velocimetry algorithm, introduced for cross correlation-based velocity data. Experiments in the wake of a cylinder at R e D = 27 000 are used to assess the suitability of the method to resolve the turbulent Kármán-Benard wake. The approach is benchmarked against traditional as well as state-of-the-art reconstruction methods, illustrating the capability of IMR of enhancing the spatial resolution of sparse velocity data.
The laminar separation bubble (LSB) that forms on the suction side of a modified NACA 64 3-618 airfoil at a chord-based Reynolds number of Re = 200 , 000 is studied using wind tunnel experiments. First, the LSB is characterized over a range of static angles of attack, in terms of the locations of separation, transition and reattachment—using surface pressure measurements, particle image velocimetry (PIV) and infrared thermography (IT). For the conditions tested, excellent agreement between the techniques is obtained. Subsequently, a pitching motion is imposed on the wind tunnel model, with reduced frequencies up to k = 0.25. While surface pressure measurements and PIV are not affected by the change in experimental conditions, the infrared approach is impaired by the thermal response of the surface. To overcome this, an extension of the differential infrared thermography (DIT) method for detecting the three characteristics of an unsteady LSB is considered. All three experimental techniques indicate a hysteresis in bubble location between the pitch up and pitch down phases of the motion, caused by the effect of the aerodynamic unsteadiness on the adverse pressure gradient. However, the DIT measurements suggest a larger hysteresis, which is attributed to the thermal response time of the model surface. The experimental results measured with the pressure sensors reveal that the hysteresis in bubble location is larger than the hysteresis in lift, indicating that the observed bubble hysteresis is not purely due to instantaneous flow conditions, but has an inherent component as well.