22 results on '"Strouhal"'
Search Results
2. Microscopic Object Classification through Passive Motion Observations with Holographic Microscopy
- Author
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Devan Rouzie, Christian Lindensmith, and Jay Nadeau
- Subjects
holographic microscopy ,Brownian motion ,Strouhal ,buoyancy ,life detection ,astrobiology ,Science - Abstract
Digital holographic microscopy provides the ability to observe throughout a volume that is large compared to its resolution without the need to actively refocus to capture the entire volume. This enables simultaneous observations of large numbers of small objects within such a volume. We have constructed a microscope that can observe a volume of 0.4 µm × 0.4 µm × 1.0 µm with submicrometer resolution (in xy) and 2 µm resolution (in z) for observation of microorganisms and minerals in liquid environments on Earth and on potential planetary missions. Because environmental samples are likely to contain mixtures of inorganics and microorganisms of comparable sizes near the resolution limit of the instrument, discrimination between living and non-living objects may be difficult. The active motion of motile organisms can be used to readily distinguish them from non-motile objects (live or inorganic), but additional methods are required to distinguish non-motile organisms and inorganic objects that are of comparable size but different composition and structure. We demonstrate the use of passive motion to make this discrimination by evaluating diffusion and buoyancy characteristics of cells, styrene beads, alumina particles, and gas-filled vesicles of micron scale in the field of view.
- Published
- 2021
- Full Text
- View/download PDF
3. The spectral signature of wind turbine wake meandering: A wind tunnel and field‐scale study.
- Author
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Heisel, Michael, Hong, Jiarong, and Guala, Michele
- Subjects
WIND turbines ,WIND tunnels ,REYNOLDS number ,WIND power plants ,ATMOSPHERIC boundary layer - Abstract
Abstract: Field‐scale and wind tunnel experiments were conducted in the 2D to 6D turbine wake region to investigate the effect of geometric and Reynolds number scaling on wake meandering. Five field deployments took place: 4 in the wake of a single 2.5‐MW wind turbine and 1 at a wind farm with numerous 2‐MW turbines. The experiments occurred under near‐neutral thermal conditions. Ground‐based lidar was used to measure wake velocities, and a vertical array of met‐mounted sonic anemometers were used to characterize inflow conditions. Laboratory tests were conducted in an atmospheric boundary layer wind tunnel for comparison with the field results. Treatment of the low‐resolution lidar measurements is discussed, including an empirical correction to velocity spectra using colocated lidar and sonic anemometer. Spectral analysis on the laboratory‐ and utility‐scale measurements confirms a meandering frequency that scales with the Strouhal number St = fD/U based on the turbine rotor diameter D. The scaling indicates the importance of the rotor‐scaled annular shear layer to the dynamics of meandering at the field scale, which is consistent with findings of previous wind tunnel and computational studies. The field and tunnel spectra also reveal a deficit in large‐scale turbulent energy, signaling a sheltering effect of the turbine, which blocks or deflects the largest flow scales of the incoming flow. Two different mechanisms for wake meandering—large scales of the incoming flow and shear instabilities at relatively smaller scales—are discussed and inferred to be related to the turbulent kinetic energy excess and deficit observed in the wake velocity spectra. [ABSTRACT FROM AUTHOR]
- Published
- 2018
- Full Text
- View/download PDF
4. Large Eddy Simulation of near-bed pipelines in oscillatory flow.
- Author
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Fonias, Efstratios N. and Grigoriadis, Dimokratis G.E.
- Subjects
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PIPELINE hydrodynamics , *LARGE eddy simulation models , *INCOMPRESSIBLE flow , *REYNOLDS number , *VORTEX shedding - Abstract
A series of unsteady, three-dimensional numerical simulations of the incompressible, oscillatory flow around a near-bed pipeline is presented. A flow at Reynolds number equal to Re α o = 20,000 with respect to the oscillatory amplitude and maximum oscillation velocity is considered. The ratio of the pipeline diameter to the oscillatory amplitude examined is in the range of D / α o = 0.1 − 1.0 , with the pipeline located at a distance of G / D = 0.0 − 1.0 . The numerical simulations are conducted by means of Large Eddy Simulation (LES), using Cartesian grids. The presence of solid boundaries is taken into account by means of the Immersed Boundary method. For turbulence modelling, two different subgrid scale models are tested, the classical Smagorinsky and the Filtered Structure Function (FSF) models. The results in terms of vortex shedding are compared against previously reported data demonstrating very good agreement. Vortex shedding patterns are presented, indicating suppression of the boundary layer separation of the lower side of the pipeline for gap lengths G / α o ≤ 1 / 20 . The characteristic values of the hydrodynamic forcing in terms of the drag and lift coefficients and the three significant oscillation frequencies extracted from the temporal variation of the forcing signals are associated with the flow regimes and wall proximity. The pipeline experiences hydrodynamic loading which is found to oscillate with the external flow frequency along the direction of the flow. Along the wall-normal direction, the forces exerted on the pipe oscillate with several frequencies of high power spectral density. However, the three significant oscillation frequencies of the lift coefficient appear to have almost constant values. The presented results can provide trends for design purposes in similar flow conditions for a wide range of engineering applications. [ABSTRACT FROM AUTHOR]
- Published
- 2018
- Full Text
- View/download PDF
5. FLOW CONTROL THROUGH VORTEX SHEDDING INTERACTION OF ONE CYLINDER DOWNSTREAM OF ANOTHER.
- Author
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Payton, Jonathan and Dakka, Sam M.
- Subjects
VORTEX shedding ,COMPUTATIONAL fluid dynamics ,ANSYS (Computer system) ,REYNOLDS number ,FLUID flow - Abstract
This study investigates the vortices produced between two 2d cylinders, and the relationship between the structures of the vortices produced at both cylinders when one is placed in the wake flow of another. CFD simulations using ANSYS Fluent were used to determine the coefficients of lift and drag, as well as the frequency of vortex shedding and size of vortices at three separate Reynolds numbers of 16000, 32000 and 65000 in different arrangements. Each arrangement of cylinders was compared against controls, which consisted of a single cylinder to determine the alteration of forces produced. Two trip wires at 7 different angles of 40, 45, 50, 55, 60, 65, and 70 degrees were then investigated at a Reynolds number of 65000 which was compared to the smooth cylinder control forces and frequency of vortex shedding. The most optimum angle of trip wires was then combined with linear cylinder arrangements also at a Reynolds number of 65000 for comparison with only the upstream cylinder utilizing the trip wires. [ABSTRACT FROM AUTHOR]
- Published
- 2017
- Full Text
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6. A CFD-FFT approach to hemoacoustics that enables degree of stenosis prediction from stethoscopic signals.
- Author
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Ali AM, Hafez AH, Elkhodary KI, and El-Morsi M
- Abstract
In this paper, we identify a new (acoustic) frequency-stenosis relation whose frequencies lie within the recommended auscultation threshold of stethoscopy (< 120 Hz). We show that this relation can be used to extend the application of phonoangiography (quantifying the degree of stenosis from bruits) to widely accessible stethoscopes. The relation is successfully identified from an analysis restricted to the acoustic signature of the von Karman vortex street, which we automatically single out by means of a metric we propose that is based on an area-weighted average of the Q-criterion for the post-stenotic region. Specifically, we perform CFD simulations on internal flow geometries that represent stenotic blood vessels of different severities. We then extract their emitted acoustic signals using the Ffowcs Williams-Hawkings equation, which we subtract from a clean signal (stenosis free) at the same heart rate. Next, we transform this differential signal to the frequency domain and carefully classify its acoustic signatures per six (stenosis-)invariant flow phases of a cardiac cycle that are newly identified in this paper. We then automatically restrict our acoustic analysis to the sounds emitted by the von Karman vortex street (phase 4) by means of our Q-criterion-based metric. Our analysis of its acoustic signature reveals a strong linear relationship between the degree of stenosis and its dominant frequency, which differs considerably from the break frequency and the heart rate (known dominant frequencies in the literature). Applying our new relation to available stethoscopic data, we find that its predictions are consistent with clinical assessment. Our finding of this linear correlation is also unlike prevalent scaling laws in the literature, which feature a small exponent (i.e., low stenosis percentage sensitivity over much of the clinical range). They hence can only distinguish mild, moderate, and severe cases. Conversely, our linear law can identify variations in the degree of stenosis sensitively and accurately for the full clinical range, thus significantly improving the utility of the relevant scaling laws... Future research will investigate incorporating the vibroacoustic role of adjacent organs to expand the clinical applicability of our findings. Extending our approach to more complex 3D stenotic morphologies and including the vibroacoustic role of surrounding organs will be explored in future research to advance the clinical reach of our findings., Competing Interests: The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper., (© 2023 The Author(s).)
- Published
- 2023
- Full Text
- View/download PDF
7. Unsteady particle tracking of micro-particle deposition in the human nasal cavity under cyclic inspiratory flow.
- Author
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Bahmanzadeh, Hojat, Abouali, Omid, and Ahmadi, Goodarz
- Subjects
- *
PARTICLE tracks (Nuclear physics) , *NASAL cavity , *AIR flow , *COMPUTATIONAL fluid dynamics , *LAGRANGIAN points , *COMPUTER simulation - Abstract
In this study, a fully unsteady computational fluid dynamics (CFD) model was used and the transient airflow properties during the entire breathing cycle, including inhalation and exhalation in a human nasal cavity, were evaluated. Unsteady particle tracking was performed to find the particle motion and deposition in the nasal airway using a Lagrangian approach. In most of earlier computer simulations, the assumption of quasi-steady or steady airflows averaged over the inhalation cycle were typically used to reduce the computational cost. In the present work particular attention was given to assessing the accuracy of these assumptions and their consequence on particle deposition in a human nasal cavity with paranasal sinuses. The simulation results for the airflow field showed significant differences between the unsteady and quasi-steady cases at low breathing rates near the beginning and end of the inspiration cycle. For breathing under a rest condition with a frequency of 0.25 Hz, the quasi-steady airflow assumption in the nasal cavity was found to be reasonable when the instantaneous Strouhal number was smaller than 0.2. The instantaneous deposition of micro-particles was also studied, and the effects of unsteady accelerating and decelerating flows on the deposition fraction were examined. The simulation results showed that the deposition fractions were affected by the accelerating and decelerating airflows during the inhalation phase. The simulated micro-particle depositions under the cyclic breathing condition were compared with those for steady breathing with an equivalent mean airflow rate. It was found that while the general trend was similar, the steady breathing simulation with the mean airflow rate during inhalation cannot accurately predict the total micro-particle deposition for cyclic breathing, particularly for 1–5 µm particles. Furthermore, the predicted regional depositions by the steady breathing were markedly different from those obtained under cyclic breathing. [ABSTRACT FROM AUTHOR]
- Published
- 2016
- Full Text
- View/download PDF
8. Appraisal of Strouhal number in wind turbine engineering.
- Author
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Trivellato, F. and Raciti Castelli, M.
- Subjects
- *
WIND turbine blades , *REYNOLDS number , *DIMENSIONLESS numbers , *FLUIDS , *APPROXIMATION theory - Abstract
Flows around blunt bodies at high Reynolds numbers generate a periodic release of staggered vortices. The dimensionless frequency of vortex shedding, the Strouhal number St , was found successful in describing periodic fluid flows. In fact, several literature datasets proved that the number St ~ 0.16 describes with reasonable (at times, excellent) approximation a large variety of periodic fluid phenomena, many of them having no clear affinity. The first motivation of the present study is to collect under one cover the results disseminated in various sources; the second purpose is to double-check the constancy of Strouhal number in wind turbines as well. The St number is here elaborated in a more informative way for horizontal-axis wind turbines, showing that it includes the tip speed ratio and the number of blades; the law St ~ 0.16 is here corroborated by further findings which includes wake meandering and the flow fields produced by three wind turbines (a two-bladed HAWT; a three-bladed lift-driven Darrieus VAWT; and a two-bladed drag-driven Savonius VAWT). The present findings suggest a design criterion for wind turbines. [ABSTRACT FROM AUTHOR]
- Published
- 2015
- Full Text
- View/download PDF
9. Wing rock phenomenon in orthotropic plates
- Author
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Pontes, Felipe da Silva, Reis, Rômulo Pierre Batista dos, Bessa, Kleiber Lima de, and Melo, José Daniel Diniz
- Subjects
Strouhal ,Wing rock ,Compósitos - Abstract
O fenômeno wing rock é caracterizado por uma oscilação rotacional indesejável em aeronaves, principalmente no eixo de rotação, que ocorre em velocidades de voo relativamente baixas e alto ângulo de ataque. As instabilidades de voo causadas por oscilações rotacionais do fenômeno wing rock podem afetar o desempenho da aeronave e o controle de voo. No presente trabalho, o fenômeno do wing rock é estudado em placas retangulares ortotrópicas de materiais compósitos com diversas razões de aspecto. Os experimentos foram realizados em um túnel de vento com velocidade do vento de 6 m/s. As placas de material compósito foram produzidas com fibras unidirecionais e posicionadas com as fibras orientadas a 0 ° ou 90 ° em relação à direção do fluxo de ar. Os parâmetros estudados foram número de Strouhal, variação do ângulo de rolagem, deformação da placa e a influência da orientação da fibra no fenômeno do wing rock. Os resultados obtidos com placas de material compósito foram comparados com resultados obtidos em placas de alumínio com mesma razão de aspecto. Observou-se para as placas compostas com fibras orientadas a 90° da direção do fluxo, com razão de aspecto de 3,25, redução das vibrações induzidas por vórtices com o aumento do ângulo de ataque, em comparação às placas de alumínio. The wing rock phenomenon is characterized by an undesirable rotational oscillation in aircrafts, mainly in roll axis, which occurs at relatively low flight speeds and high angle of attack. Flight instabilities caused by rotational oscillations of the wing rock phenomenon can affect aircraft performance and flight control. In the present work, the wing rock phenomenon is studied in rectangular orthotropic plates of composite materials with several elongations. The experiments were performed in a wind tunnel with a wind speed of 6 m/s. Composite material plates were produced with unidirectional fibers and were positioned with the fibers oriented at 0° or 90° with respect to the air flow direction. The parameters studied were Strouhal number, variation of the rolling angle, plate deformation and the influence of the fiber orientation on the wing rock phenomenon. The results obtained with composite material plates were compared with results obtained in aluminum plates with the same elongation. It was observed for the composite plates with fibers oriented at 90° of the flow direction, with aspect ratio of 3.25, a reduction in vibrations induced by vortices as the angle of attack increases, as compared to aluminum plates.
- Published
- 2020
10. Evaluation of wind loads on super-tall buildings from field-measured wind-induced acceleration response.
- Author
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Xu, A., Xie, Z. N., Fu, J. Y., Wu, J. R., and Tuan, Alex
- Subjects
TALL buildings ,WIND pressure ,SKYSCRAPERS ,ACCELERATION (Mechanics) ,WINDS ,VELOCITY - Abstract
SUMMARY With the nonstationary wind-induced acceleration data from full-scale measurements, an approach for estimation of the wind-induced overturning bending moments for super-tall buildings was proposed in this paper. The empirical mode decomposition was employed to decompose the measured acceleration data into a set of intrinsic mode functions and a residual component. To remove the baseline offset, the residual component and the intrinsic mode function components with long-period were eliminated before their integrations into velocity and displacement components. Then, the intrinsic mode function components, which have the same dominant periods as the natural periods of the studied tall buildings, were extracted from the original signals, and the natural frequency and damping ratio for the first vibration mode of the building were identified. Finally, the wind-induced overturning bending moments of the building were obtained from the generalized wind loads for the first vibration mode, which could be obtained from the time history analysis of dynamic equation. The Hilbert spectrum of wind-induced overturning bending moments was utilized to observe its characteristics in both time and frequency domains, and the Strouhal number was thus identified. The proposed scheme and some selected results may be helpful for further understanding of wind effects on super-tall buildings. Copyright © 2012 John Wiley & Sons, Ltd. [ABSTRACT FROM AUTHOR]
- Published
- 2014
- Full Text
- View/download PDF
11. Flow-body interaction, self-induced resonant vibrations by vortex shedding on a bladeless wind turbine of materials with high electromechanical couplinginteracción
- Author
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Grau Moreso, Alba
- Subjects
Bladeless wind turbine ,Acoplamiento electromecánico ,Wind gradient ,Resonancia ,Calle de vórtices ,Electromechanical coupling ,Perfil vertical de viento ,Strouhal ,INGENIERIA AEROESPACIAL ,Flutter ,Resonance ,Flameo (flutter) ,Interacción fluido-estructura ,Fluid-structure interaction ,Aerogenerador sin aspas ,Grado en Ingeniería Aeroespacial-Grau en Enginyeria Aeroespacial ,Vortex street - Abstract
[ES] En el siguiente trabajo ha sido realizado un análisis teórico del aerogenerador sin aspas inventado recientemente por Vortex Bladeless S.L. La aerodinámica y vibraciones mecánicas en él son estudiadas, así como la función de los materiales con alto acoplamiento electromecánico en este dispositivo. El aerogenerador estudiado funciona gracias a vibraciones resonantes auto-excitadas por la calle de vórtices desarrollada aguas abajo de la estructura. La energía aeroelástica absorbida es transformada en energía eléctrica a través de los materiales con alto acoplamiento electromecánico con los cuales está construida la estructura. El estudio comienza con la generación inicial de vórtices en el caso estacionario. La calle de vórtices y las fuerzas del fluido sobre un cilindro son analizadas y se ha realizado también un símil entre el aerogenerador y el flujo alrededor de edificios altos. La literatura disponible sobre el número de Strouhal en aerogeneradores es revisada y también observamos la importancia del perfil vertical de viento en nuestro análisis. Seguidamente, se estudia la interacción entre la vibración de un cilindro y la calle de vórtices generada tras él. El desarrollo de los vórtices cambia y con ello, las fuerzas del fluido sobre la estructura. Analizamos el efecto de la resonancia y la consecuente inestabilidad aeroelástica, el flameo, que es el efecto buscado en el aerogenerador estudiado para maximizar la absorción de energía. Para finalizar el proceso, se transforma la energía mecánica de la oscilación de la estructura en energía eléctrica a través de los materiales con alto acoplamiento electromecánico de la estructura. Se analiza por último otra función de estos materiales en el aerogenerador, la modulación de la frecuencia natural de la estructura por medio de la entrada de voltaje elegida. Finalmente, se ha realizado una introducción del software FSI, cuya función es realizar análisis computacionales en problemas de interacción fluido-estructura. Estos problemas aparecen en numerosas aplicaciones de la ingeniería y la arquitectura., [EN] A theoretical analysis of the bladeless wind turbine, recently invented by Vortex Bladeless S.L., is presented. The aerodynamics and vibrations involved are studied, as well as the function of materials with high electromechanical coupling on this device. The wind turbine studied works thanks to resonant vibrations self-excited by the vortex street developed downwash the structure. The aeroelastic energy absorbed is transformed into electrical energy due to the high electromechanical coupling of the materials the structure is built with. The study begins with the initial vortex generation on the stationary case. The vortex street and the fluid forces on a cylinder are analysed and a simile of the device and the flow around tall buildings is made. The literature available about the Strouhal number on wind turbines is revised and the importance of the wind gradient in wind engineering is also observed. Then the interaction between the vibration of a cylinder and the vortex street generated is studied. The vortices development changes and with that, the fluid forces over the structure too. We study the resonance effect and with it, the aeroelastic instability, flutter, which is the objective of the device in order to maximize the energy absorption. To finish the process, the transformation of the mechanical energy from the oscillation into usable electrical energy is performed through the high electromechanical coupling of the materials of the structure. This function of the materials, and the modulation of the natural frequency of the structure by modifying the voltage input are analysed. Finally, an introduction of the basis of a software (FSI) to perform computational analysis of fluid-structure interaction problems is presented, as these problems are shown in many engineering and architecture applications.
- Published
- 2020
12. Flow-body interaction, self-induced resonant vibrations by vortex shedding on a bladeless wind turbine of materials with high electromechanical couplinginteracción
- Author
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Hoyas Calvo, Sergio, Cerón Muñoz, Hernán, Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics, Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny, Grau Moreso, Alba, Hoyas Calvo, Sergio, Cerón Muñoz, Hernán, Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics, Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny, and Grau Moreso, Alba
- Abstract
[ES] En el siguiente trabajo ha sido realizado un análisis teórico del aerogenerador sin aspas inventado recientemente por Vortex Bladeless S.L. La aerodinámica y vibraciones mecánicas en él son estudiadas, así como la función de los materiales con alto acoplamiento electromecánico en este dispositivo. El aerogenerador estudiado funciona gracias a vibraciones resonantes auto-excitadas por la calle de vórtices desarrollada aguas abajo de la estructura. La energía aeroelástica absorbida es transformada en energía eléctrica a través de los materiales con alto acoplamiento electromecánico con los cuales está construida la estructura. El estudio comienza con la generación inicial de vórtices en el caso estacionario. La calle de vórtices y las fuerzas del fluido sobre un cilindro son analizadas y se ha realizado también un símil entre el aerogenerador y el flujo alrededor de edificios altos. La literatura disponible sobre el número de Strouhal en aerogeneradores es revisada y también observamos la importancia del perfil vertical de viento en nuestro análisis. Seguidamente, se estudia la interacción entre la vibración de un cilindro y la calle de vórtices generada tras él. El desarrollo de los vórtices cambia y con ello, las fuerzas del fluido sobre la estructura. Analizamos el efecto de la resonancia y la consecuente inestabilidad aeroelástica, el flameo, que es el efecto buscado en el aerogenerador estudiado para maximizar la absorción de energía. Para finalizar el proceso, se transforma la energía mecánica de la oscilación de la estructura en energía eléctrica a través de los materiales con alto acoplamiento electromecánico de la estructura. Se analiza por último otra función de estos materiales en el aerogenerador, la modulación de la frecuencia natural de la estructura por medio de la entrada de voltaje elegida. Finalmente, se ha realizado una introducción del software FSI, cuya función es realizar análisis computacionales en problemas de interacción fluido-estructura, [EN] A theoretical analysis of the bladeless wind turbine, recently invented by Vortex Bladeless S.L., is presented. The aerodynamics and vibrations involved are studied, as well as the function of materials with high electromechanical coupling on this device. The wind turbine studied works thanks to resonant vibrations self-excited by the vortex street developed downwash the structure. The aeroelastic energy absorbed is transformed into electrical energy due to the high electromechanical coupling of the materials the structure is built with. The study begins with the initial vortex generation on the stationary case. The vortex street and the fluid forces on a cylinder are analysed and a simile of the device and the flow around tall buildings is made. The literature available about the Strouhal number on wind turbines is revised and the importance of the wind gradient in wind engineering is also observed. Then the interaction between the vibration of a cylinder and the vortex street generated is studied. The vortices development changes and with that, the fluid forces over the structure too. We study the resonance effect and with it, the aeroelastic instability, flutter, which is the objective of the device in order to maximize the energy absorption. To finish the process, the transformation of the mechanical energy from the oscillation into usable electrical energy is performed through the high electromechanical coupling of the materials of the structure. This function of the materials, and the modulation of the natural frequency of the structure by modifying the voltage input are analysed. Finally, an introduction of the basis of a software (FSI) to perform computational analysis of fluid-structure interaction problems is presented, as these problems are shown in many engineering and architecture applications.
- Published
- 2020
13. Aerodynamic force evaluation for ice shedding phenomenon using vortex in cell scheme, penalisation and level set approaches.
- Author
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Morency, F., Beaugendre, H., and Gallizio, F.
- Subjects
- *
AERODYNAMIC load , *VORTEX shedding , *ICE , *LEVEL set methods , *BOUNDARY value problems , *SIMULATION methods & models , *AIRPLANES - Abstract
In this work, we propose a formulation to evaluate aerodynamic forces for flow solutions based on Cartesian grids, penalisation and level set functions. The formulation enables the evaluation of forces on closed bodies moving at different velocities. The use of Cartesian grids bypasses the meshing issues, and penalisation is an efficient alternative to explicitly impose boundary conditions so that the body fitted meshes can be avoided. Penalisation enables ice shedding simulations that take into account ice piece effects on the flow. Level set functions describe the geometry in a non-parametric way so that geometrical and topological changes resulting from physics, and particularly shed ice pieces, are straightforward to follow. The results obtained with the present force formulation are validated against other numerical formulations for circular and square cylinder in laminar flow. The capabilities of the proposed formulation are demonstrated on ice trajectory calculations for highly separated flow behind a bluff body, representative of inflight aircraft ice shedding. [ABSTRACT FROM AUTHOR]
- Published
- 2012
- Full Text
- View/download PDF
14. Application of RES methods for computation of hydrodynamic flows by an example of a 2D flow past a circular cylinder for Re=5–200
- Author
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Kozlov, Igor M., Dobrego, Kirill V., and Gnesdilov, Nickolai N.
- Subjects
- *
SIMULATION methods & models , *HYDRODYNAMICS , *TWO-phase flow , *THERMODYNAMICS of engine cylinders , *MACH number , *FOURIER transforms , *POISSON'S equation , *VISCOSITY - Abstract
Abstract: An effective method of simulation of multidimensional hydrodynamic problems for small Mach numbers is described. The method is based on utilization of FFT (fast Fourier transform) for solving the Poisson equation on a rectangular grid in domains with complicated geometry (particularly multi-linked). Simulation was performed with zero numerical viscosity. The speed of calculation of the Poisson equation is 1–2 orders of magnitude higher compared to that of the calculation based on standard iteration techniques. Systematic simulations of a 2D flow past a cylinder in the channel with permeable and impermeable boundaries were performed. The critical values of the Re number of the onset of vortex movement (Re0) and loss of stability of steady (Re1) and two-dimensional movement (Re2) are estimated with high accuracy for the two cases mentioned. [ABSTRACT FROM AUTHOR]
- Published
- 2011
- Full Text
- View/download PDF
15. Dynamic similarity during human running: About Froude and Strouhal dimensionless numbers
- Author
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Delattre, Nicolas, Lafortune, Mario A., and Moretto, Pierre
- Subjects
- *
RUNNING , *SIMILARITY (Physics) , *ANTHROPOMETRY , *NUMERICAL analysis , *HUMAN mechanics , *BIOMECHANICS - Abstract
Abstract: Dynamic similarity is a widely used concept in the fluid mechanics field, and consists in placing two different-sized systems in equivalent experimental conditions. This enables removal of the effects of size and prediction of the behavior of a full size system from a scale model. The aim of this study was to test whether the Froude number (Nfr) or the Strouhal number (Str) could be used as a criterion for dynamic similarity during running. Fifteen male subjects ran barefoot on a runway in three experimental conditions (i) all subjects ran at the same speed V=3.5ms−1; (ii) the speed was determined from Nfr; (iii) the stride frequency was determined from Str. Antero-posterior (Fy) and vertical (Fz) ground reaction force components were assessed. The similarity between the subjects was analysed from scale factor sets computed from anthropometric and kinetic data. The use of Str implied strong inter-subject similarity for temporal parameters (mean r=0.96, time to Fz peak, time to Fy braking peak, Fy zero fore–aft shear, time to Fy propulsive peak) while Nfr induced fewer and lower similarities (mean r=0.75, Fy zero fore–aft shear, time to Fy propulsive peak, Fy braking impulse) that only concerned antero-posterior parameters. This study brought experimental evidence that neither Nfr nor Str were sufficient for dynamic similarity during running, but that each of them made its own contribution. These findings suggested that the concomitant use of Nfr and Str should be assessed to induce inter-subject dynamic similarity during running. [Copyright &y& Elsevier]
- Published
- 2009
- Full Text
- View/download PDF
16. Flujo en placas planas normales en tándem: Estudio de la dependencia del número de Strouhal con el bloqueo
- Author
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Carreres Talens, Marcos, Zanotti, Alex, Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics, Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny, León Ilaño, Marcos Alexander, Carreres Talens, Marcos, Zanotti, Alex, Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics, Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny, and León Ilaño, Marcos Alexander
- Abstract
[ES] El objetivo de este trabajo es la medida del flujo alrededor de placas en tándem normales a la corriente libre usando dos diferentes bloqueos. La realización de los experimentos se lleva a cabo en un túnel de viento de ciclo cerrado a un Reynolds fijo Re = 22400 con dos pares de placas de diferente cuerda para controlar el bloqueo. Las medidas son tomadas con un anemómetro de hilo caliente para diferentes distancias de separación entre placas. De esta manera se puede obtener la relación entre el número de Strouhal y la distancia de separación. Un estudio adicional se lleva a cabo a Re = 83500 para un estudio más profundo del bloqueo mayor. Para la correcta visualización de los resultados experimentales, se lleva a cabo un estudio paramétrico de la representación de la transformada de Fourier. Se pretende determinar la influencia del ratio de bloqueo y los grupos adimensionales (Strouhal y Reynolds) en el fenómeno estudiado., [EN] The aim of this work is the measurement of flow around flat plates in tandem normal to the free stream using two different blockage ratios. The conducting of the experiments is carried out in a closed return wind tunnel at a fixed Reynolds number Re = 22400 with two pairs of plates of different chord in order to change the blockage. The measurements are taken with a hot wire anemometer at the back of the downstream plate for different spacing distances between plates. Thus the relation between the Strouhal number and the separation distance can be found. An additional test is carried out at Re = 83500 for a deeper study of the largest blockage. For a correct visualization of experimental results, a prametric study of the Fourier Transform representation is performed. This investigation allows to determine the influence of the blockage ratio and the non-dimensional groups in the studied phenomena.
- Published
- 2019
17. Flujo en placas planas normales en tándem: Estudio de la dependencia del número de Strouhal con el bloqueo
- Author
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León Ilaño, Marcos Alexander
- Subjects
Tándem ,Fourier Transform ,Strouhal ,Vortex shedding frequency ,Transformada de Fourier ,Grado en Ingeniería Aeroespacial-Grau en Enginyeria Aeroespacial ,INGENIERIA AEROESPACIAL ,Blockage ratio ,Frecuencia de desprendimiento de vórtice ,Flat plates ,Tandem ,Wind tunnel - Abstract
[ES] El objetivo de este trabajo es la medida del flujo alrededor de placas en tándem normales a la corriente libre usando dos diferentes bloqueos. La realización de los experimentos se lleva a cabo en un túnel de viento de ciclo cerrado a un Reynolds fijo Re = 22400 con dos pares de placas de diferente cuerda para controlar el bloqueo. Las medidas son tomadas con un anemómetro de hilo caliente para diferentes distancias de separación entre placas. De esta manera se puede obtener la relación entre el número de Strouhal y la distancia de separación. Un estudio adicional se lleva a cabo a Re = 83500 para un estudio más profundo del bloqueo mayor. Para la correcta visualización de los resultados experimentales, se lleva a cabo un estudio paramétrico de la representación de la transformada de Fourier. Se pretende determinar la influencia del ratio de bloqueo y los grupos adimensionales (Strouhal y Reynolds) en el fenómeno estudiado., [EN] The aim of this work is the measurement of flow around flat plates in tandem normal to the free stream using two different blockage ratios. The conducting of the experiments is carried out in a closed return wind tunnel at a fixed Reynolds number Re = 22400 with two pairs of plates of different chord in order to change the blockage. The measurements are taken with a hot wire anemometer at the back of the downstream plate for different spacing distances between plates. Thus the relation between the Strouhal number and the separation distance can be found. An additional test is carried out at Re = 83500 for a deeper study of the largest blockage. For a correct visualization of experimental results, a prametric study of the Fourier Transform representation is performed. This investigation allows to determine the influence of the blockage ratio and the non-dimensional groups in the studied phenomena.
- Published
- 2019
18. Microscopic Object Classification through Passive Motion Observations with Holographic Microscopy.
- Author
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Rouzie, Devan, Lindensmith, Christian, and Nadeau, Jay
- Subjects
DIGITAL holographic microscopy ,MICROSCOPY ,ENVIRONMENTAL sampling ,BUOYANCY ,BROWNIAN motion - Abstract
Digital holographic microscopy provides the ability to observe throughout a volume that is large compared to its resolution without the need to actively refocus to capture the entire volume. This enables simultaneous observations of large numbers of small objects within such a volume. We have constructed a microscope that can observe a volume of 0.4 µm × 0.4 µm × 1.0 µm with submicrometer resolution (in xy) and 2 µm resolution (in z) for observation of microorganisms and minerals in liquid environments on Earth and on potential planetary missions. Because environmental samples are likely to contain mixtures of inorganics and microorganisms of comparable sizes near the resolution limit of the instrument, discrimination between living and non-living objects may be difficult. The active motion of motile organisms can be used to readily distinguish them from non-motile objects (live or inorganic), but additional methods are required to distinguish non-motile organisms and inorganic objects that are of comparable size but different composition and structure. We demonstrate the use of passive motion to make this discrimination by evaluating diffusion and buoyancy characteristics of cells, styrene beads, alumina particles, and gas-filled vesicles of micron scale in the field of view. [ABSTRACT FROM AUTHOR]
- Published
- 2021
- Full Text
- View/download PDF
19. Aerodynamic force evaluation for ice shedding phenomenon using vortex in cell scheme, penalisation and level set approaches
- Author
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Federico Gallizio, François Morency, Héloïse Beaugendre, Ecole de Technologie Supérieure [Montréal] (ETS), Parallel tools for Numerical Algorithms and Resolution of essentially Hyperbolic problems (BACCHUS), Inria Bordeaux - Sud-Ouest, Institut National de Recherche en Informatique et en Automatique (Inria)-Institut National de Recherche en Informatique et en Automatique (Inria)-Université de Bordeaux (UB)-Centre National de la Recherche Scientifique (CNRS), Institut de Mathématiques de Bordeaux (IMB), Université Bordeaux Segalen - Bordeaux 2-Université Sciences et Technologies - Bordeaux 1 (UB)-Université de Bordeaux (UB)-Institut Polytechnique de Bordeaux (Bordeaux INP)-Centre National de la Recherche Scientifique (CNRS), Dipartimento di Automatica e Informatica [Torino] (DAUIN), Politecnico di Torino = Polytechnic of Turin (Polito), plafrim, Centre National de la Recherche Scientifique (CNRS)-Université de Bordeaux (UB)-Inria Bordeaux - Sud-Ouest, Institut National de Recherche en Informatique et en Automatique (Inria)-Institut National de Recherche en Informatique et en Automatique (Inria), and Université Bordeaux Segalen - Bordeaux 2-Université Sciences et Technologies - Bordeaux 1-Université de Bordeaux (UB)-Institut Polytechnique de Bordeaux (Bordeaux INP)-Centre National de la Recherche Scientifique (CNRS)
- Subjects
Computational Mechanics ,Energy Engineering and Power Technology ,Aerospace Engineering ,[PHYS.MECA.GEME]Physics [physics]/Mechanics [physics]/Mechanical engineering [physics.class-ph] ,aerodynamic force ,01 natural sciences ,ACM: G.: Mathematics of Computing ,010305 fluids & plasmas ,law.invention ,[SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph] ,Physics::Fluid Dynamics ,ice shedding ,Level set ,law ,0103 physical sciences ,circular cylinder ,Cartesian coordinate system ,Boundary value problem ,[PHYS.MECA.MEFL]Physics [physics]/Mechanics [physics]/Fluid mechanics [physics.class-ph] ,0101 mathematics ,VIC scheme ,Trajectory (fluid mechanics) ,ACM: J.: Computer Applications/J.2: PHYSICAL SCIENCES AND ENGINEERING ,aircraft icing ,Mechanical Engineering ,Strouhal ,Laminar flow ,penalisation ,Mechanics ,Condensed Matter Physics ,[INFO.INFO-MO]Computer Science [cs]/Modeling and Simulation ,Vortex ,[SPI.MECA.GEME]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanical engineering [physics.class-ph] ,010101 applied mathematics ,Aerodynamic force ,Classical mechanics ,Flow (mathematics) ,ACM: I.: Computing Methodologies/I.6: SIMULATION AND MODELING ,Mechanics of Materials ,square cylinder ,level set - Abstract
International audience; In this work, we propose a formulation to evaluate aerodynamic forces for flow solutions based on Cartesian grids, penalisation and level set functions. The formulation enables the evaluation of forces on closed bodies moving at different velocities. The use of Cartesian grids bypasses the meshing issues, and penalisation is an efficient alternative to explicitly impose boundary conditions so that the body fitted meshes can be avoided. Penalisation enables ice shedding simulations that take into account ice piece effects on the flow. Level set functions describe the geometry in a non-parametric way so that geometrical and topological changes resulting from physics, and particularly shed ice pieces, are straightforward to follow. The results obtained with the present force formulation are validated against other numerical formulations for circular and square cylinder in laminar flow. The capabilities of the proposed formulation are demonstrated on ice trajectory calculations for highly separated flow behind a bluff body, representative of inflight aircraft ice shedding.
- Published
- 2012
- Full Text
- View/download PDF
20. Estudio numérico y experimental del flujo a sotavento de un modelo de barrera eólica porosa
- Author
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Bacchi, Federico, Marañón Di Leo, Julio, Delnero, Juan Sebastián, and Giacopinelli, Pablo Esteban Luis
- Subjects
Turbulencia ,Strouhal ,K-omega ,Barreras eólicas ,Ingeniería Aeronáutica - Abstract
En este trabajo se analiza en forma numérica y experimental el flujo a sotavento de una barrera eólica porosa en el túnel de viento de capa límite del Área Departamental Aeronáutica. Se miden y calculan numéricamente las velocidades instantáneas y se comparan distribuciones espaciales de velocidad media y frecuencias de desprendimientos periódicos entre los experimentos y los resultados de simulaciones con dos modelos de turbulencia de dos ecuaciones: k-omega y k-epsilon. Se demuestra que el modelo k-omega es capaz de reproducir con muy buena aproximación las características del flujo detrás de la barrera, mientras que los resultados del modelo k-epsilon presentan discrepancias significativas en algunos puntos., Grupo Fluidodinámica Computacional
- Published
- 2008
21. Froude and Strouhal dimensionless numbers to study human gait: an experimental approach.
- Author
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Villeger, D., Delattre, N., Watier, B., and Moretto, P.
- Subjects
- *
DIMENSIONLESS numbers , *RUNNING , *WALKING , *TRACKS (Athletics) , *PHYSICAL measurements - Abstract
The article presents a study which aims to develop a contaminant of Froude number (Nfr) and Strouhal number (Str) for an accurate dimensionless human walking and running analysis. It states that a light running track was used to identify the speed of the subjects. Results show that the walk-to-run transition occurs nearly 0.5 value of the Nfr.
- Published
- 2012
- Full Text
- View/download PDF
22. Sidetone generator flowmeter
- Author
-
Fritz, Robert [Schenectady, NY]
- Published
- 1986
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