Relevant bibliographies by topics / Physics of flow

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Physics of flow'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Physics of flow"

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Javadi, Khodayar, Hamid Moezzi-Rafie, Vahid Goodarzi-Ardakani, Aliyar Javadi, and Reinhard Miller. "Flow physics exploration of surface tension driven flows." Colloids and Surfaces A: Physicochemical and Engineering Aspects 518 (April 2017): 30–45. http://dx.doi.org/10.1016/j.colsurfa.2016.12.030.

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Sharma, H., A. Vashishtha, and E. Rathakrishnan. "Twin-vortex flow physics." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 222, no. 6 (June 2008): 783–88. http://dx.doi.org/10.1243/09544100jaero322.

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Zamir,, M., and RS Budwig,. "Physics of Pulsatile Flow." Applied Mechanics Reviews 55, no. 2 (March 1, 2002): B35. http://dx.doi.org/10.1115/1.1451229.

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Schadschneider, Andreas. "Statistical physics of traffic flow." Physica A: Statistical Mechanics and its Applications 285, no. 1-2 (September 2000): 101–20. http://dx.doi.org/10.1016/s0378-4371(00)00274-0.

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Harwood, C. M., and Y. L. Young. "A physics-based gap-flow model for potential flow solvers." Ocean Engineering 88 (September 2014): 578–87. http://dx.doi.org/10.1016/j.oceaneng.2014.03.025.

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Viti, Valerio, Reece Neel, and Joseph A. Schetz. "Detailed flow physics of the supersonic jet interaction flow field." Physics of Fluids 21, no. 4 (April 2009): 046101. http://dx.doi.org/10.1063/1.3112736.

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Elíasson, Jόnas, and Þorsteinn Sæmundsson. "Physics and Modeling of Various Hazardous Landslides." Geosciences 11, no. 3 (March 1, 2021): 108. http://dx.doi.org/10.3390/geosciences11030108.

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In 2014, the Varnes classification system for landslides was updated. Complex landslides can still be a problem to classify as the classification does not include the flow type in the hydrodynamical sense. Three examples of Icelandic landslides are presented and later used as case studies in order to demonstrate the methods suggested to analyze the flow. The methods are based on the different physical properties of the flow types of the slides. Three different flow types are presented, named type (i), (ii), and (iii). Types (i) and (ii) do not include turbulent flows and their flow paths are sometimes independent of the velocity. Type (iii) include high velocity flows; they are treated with the translator wave theory, where a new type of a slope factor is used. It allows the slide to stop when the slope has flattened out to the value that corresponds to the stable slope property of the flowing material. The type studies are for a fast slide of this type, also a large slip circle slide that turns into a fast-flowing slide farther down the path and finally a large slide running so fast that it can run for a kilometer on flat land where it stops with a steep front.
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Nakajima, Yoshikazu, Hiroshi Inomata, Hiroki Nogawa, Yohshinobu Sato, Shinichi Tamura, Kozo Okazaki, and Seiji Torii. "Physics-based flow estimation of fluids." Pattern Recognition 36, no. 5 (May 2003): 1203–12. http://dx.doi.org/10.1016/s0031-3203(02)00078-x.

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Gierens, K., B. Kärcher, H. Mannstein, and B. Mayer. "Aerodynamic Contrails: Phenomenology and Flow Physics." Journal of the Atmospheric Sciences 66, no. 2 (February 1, 2009): 217–26. http://dx.doi.org/10.1175/2008jas2767.1.

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Abstract Aerodynamic contrails have been recognized for a long time although they appear sporadically. Usually one observes them under humid conditions near the ground, where they are short-lived phenomena. Aerodynamic contrails appear also at cruise levels where they may persist when the ambient atmosphere is ice-supersaturated. The present paper presents a theoretical investigation of aerodynamic contrails in the upper troposphere. The required flow physics are explained and applied to a case study. Results show that the flow over aircraft wings leads to large variations of pressure and temperature. Average pressure differences between the upper and lower sides of a wing are on the order of 50 hPa, which is a quite substantial fraction of cruise-level atmospheric pressures. Adiabatic cooling exceeds 20 K about 2 m above the wing in a case study shown here. Accordingly, extremely high supersaturations (exceeding 1000%) occur for a fraction of a second. The potential consequences for the ice microphysics are discussed. Because aerodynamic contrails are independent of the formation conditions of jet contrails, they form an additional class of contrails that might be complementary because they form predominantly in layers that are too warm for jet contrail formation.
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Ghosh, S. K. "The physics of deformation and flow." Journal of Mechanical Working Technology 12, no. 1 (November 1985): 120. http://dx.doi.org/10.1016/0378-3804(85)90049-x.

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Dissertations / Theses on the topic "Physics of flow"

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Basnet, Keshav. "Flow around porous barriers: fundamental flow physics and applications." Diss., University of Iowa, 2015. https://ir.uiowa.edu/etd/1824.

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Investigating flow and turbulence structure around a barrier mounted on the ground or placed in its vicinity is a fundamental problem in wind engineering because of many practical applications related to protection against adverse effects induced by major wind storms (e.g., hurricanes) and snow events (e.g., snow fences used to reduce adverse effects of snow drifting on the roads). In this work the focus is on the case when the obstacle/barrier is porous and the shape of the obstacle is close to a high-aspect-ratio rectangular cylinder situated in the vicinity of the ground. The study employs a range of numerical and experimental techniques to achieve this goal that include 3D LES and 2D RANS numerical simulations, and RTK survey and 3D photogrammetry techniques to measure ground elevations and snow deposits in the field. In the first part of the study, high-resolution large eddy simulations are used to understand the fundamental flow physics of flow past 2D solid and porous vertical plates with a special focus on describing the unsteady wind loads on the obstacle, vortical structure of the turbulent wake, spectral content of the wake, the separated shear layers and of the characteristics of the large-scale vortex shedding behind the plate, if present. Results show that LES can accurately predict mean flow and turbulence statistics around solid/porous cylinders. Then, a detailed parametric study of flow past vertical solid and porous plates situated in the vicinity of a horizontal bed is performed for the purpose of understanding changes in the mean flow structure, turbulence statistics and dynamics of large scale coherent structures as a function of the main nondimensional geometrical parameters (bottom gap for solid and porous plates, and porosity and average hole size of porous plates) and flow variables (e.g., bed roughness) that affect the wake flow. In particular, the LES flow fields allowed clarifying how the interactions between the bottom and the top separated shear layers change with increasing bottom gap and what is the effect of the bleeding flow on the interactions between the separated shear layers that determine the coherence of the large-scale eddies at large distances from the wake. In the second part of the thesis, a novel methodology based on field monitoring of the snow deposits and RANS numerical simulations is proposed to improve the design of snow fences and in particular the design of lightweight plastic snow fences that are commonly used to protect roads in the US Midwest against the snow drifting. The goal of the design optimization procedure is to propose a snow fence design that can retain a considerable amount of snow within a shorter downwind distance compared to fences of standard design. A major contribution of the present thesis was the development of a novel non-intrusive image-based technique that can be used to quantitatively estimate the temporal evolution of the volume of snow trapped by a fence over long periods of time. This technique is based on 3-D close range photogrammetry. Results showed that this technique can produce estimations of the snow deposits of comparable accuracy to that given by commonly used methods. This is the first application of this type of techniques to measurements of the snow deposits.
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Paleo, Cageao Paloma. "Fluid-particle interaction in geophysical flows : debris flow." Thesis, University of Nottingham, 2014. http://eprints.nottingham.ac.uk/27808/.

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Small scale laboratory experiments were conducted to study the dynamic mor- phology and rheological behaviour of fluid-particle mixtures, such as snout-body architecture, levee formation, deposition and particle segregation effects. Debris flows consist of an agitated mixture of rock and sediment saturated with water. They are mobilized under the influence of gravity from hill slopes and channels and can reach long run-out distance and have extremely destructive power. Better understanding of the mechanisms that govern these flows is required to assess and mitigate the hazard of debris flows and similar geophysical flows. Debris flow models are required to accurately deal with evolving behaviours in space and time, to be able to predict flow height, velocity profiles and run-out distances and shapes. The evolution of laboratory debris flows, both dry glass beads and mixtures with water or glycerol, released from behind a lock gate to flow down an inclined flume, was observed through the channel side wall and captured with high speed video and PIV analysis to provide velocity profiles through out the flow depth. Pore pressure and the normal and shear stress at the base of the flow were also measured. Distinct regions were characterized by the non-fluctuating region and the in- termittent granular cloud surrounding the flows. The extent of these regions was shown to be related to flow properties. The separation of these two regions allowed the systematic definition of bulk flow characteristics such as characteristic height and flow front position. Laboratory flows showed variations in morphology and rheological characteristics under the influence of particle size, roughness element diameter, interstitial fluid viscosity and solid volume fraction. Mono-dispersed and poly-dispersed components mixed with liquids without fine sediments, reveal a head and body structure and an appearance similar to the classic anatomy of real debris flows. Unsaturated fronts were observed in mono-dispersed flows, suggesting that particle segregation is not the only mechanism. A numerical simulation of laboratory debris flows using the computer model RAMMS (RApid Mass Movements Simulation) was tested with dry laboratory flows, showing close similarity to calculated mean velocities.
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Pathmathas, Thirunavukkarasu. "Granular flow modelling of rotating drum flows using positron emission particle tracking." Doctoral thesis, University of Cape Town, 2015. http://hdl.handle.net/11427/15707.

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Tumbling mills are characterized by a flowing granular mixture comprising slurry, ore and grinding media. Akin to fluid flow, a rheological description underpinning granular flow has long been expected and pursued by many researchers. Unfortunately, no single theory has hitherto been able to successfully describe all the peculiar features and flow phases of granular systems. Tumbling mills exhibit a rich coexistence of all known flow phases and is arguably the most complicated of the granular flow geometries. Not surprisingly, current comminution models are almost entirely empirical with limited predictive capability beyond their window of design. Using Positron Emission Particle Tracking (PEPT) data we recover the key ingredients (velocity, shear rate, volume concentration, bed depth) for developing, testing and calibrating granular flow models. In this regard, 5 mm and 8 mm glass beads are rotated within a 476 mm diameter mill, fitted with angled lifter bars along the inner azimuthal walls and operated in batch mode across a range of drum rotation speeds that span cascading and cataracting Froude regimes. After averaging the PEPT outputs into representative volume elements, subsequent continuum analysis of the flowing layer revealed a rich coexistence of flow regimes - (i) quasi-static, (ii) dense (liquid-like), and (iii) inertial - that are consistent with the measured volume concentrations spanning these regimes in rotating drums. Appropriately matched constitutive choices for the shear stresses then facilitated the derivation of a new granular rheology that is able to (smoothly) capture all phases of the tumbling mill flow at transition points that match leading experimental findings reported in the literature. Limiting our models to athermal boundary conditions, we then derive the power density for better understanding of flow dissipation that ultimately drives the comminution purpose of tumbling mills. The rheology and power density models were then applied to the 5 mm and 8 mm glass bead data to reveal that shear power density is an order of magnitude larger than the normal component. Notwithstanding, the effective friction coefficient - which is akin to viscosity in typical fluids - remains relatively constant across most of the flowing layer with notable exponential growth across the interface from dense-to-inertial that continued into the inertial regime.
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Bradshaw, Sean D. (Sean Darien) 1978. "Physics-based, reduced-order combustor flow modeling." Thesis, Massachusetts Institute of Technology, 2002. http://hdl.handle.net/1721.1/82215.

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Qazi, S. Junaid S. "Flow of Colloidal Mesophases." Doctoral thesis, Uppsala universitet, Materialfysik, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-152872.

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This dissertation presents new work and results in the flow of complex fluids and experimental methodologies for their investigation. Plate-like colloidal particles of kaolinite and nickel hydroxide are studied. A study of lamellar fragments and their mixture with the nickel hydroxide particles is also presented. The lamellar fragments are self-assembled structures of surfactant molecules that approximate disks. Particles are seen to align with their large faces parallel to the flow direction under shear and elongational strains. Order parameters have been calculated to quantify the extent of preferential alignment and direction of orientation. The experimental data are supported by comparisons with finite-element fluid mechanics calculations that provide estimates of the flow patterns and the strain rates. Elongational strain rates in the range of 5 − 20 s−1 are required to induce a high degree of alignment with the various sizes of the particles whereas about two to three order of magnitude higher shear strain rates are required. The combination of both elongational and shear strain is an effective means to provide a uniform alignment. Comparison of the Peclet numbers calculated for both the shear and elongational flow are presented and this explains that alignment occurs when the energy per particle of the strain is larger than the thermal energy. Mixtures have shown complex behavior: significant changes in the structure are observed that are not seen to the same extent in samples at rest. X-ray diffraction and small-angle neutron scattering techniques are used to characterize the samples and determine the structure in flowing systems. Laboratory X-ray diffraction can be used to characterize dispersed samples. The combination of dynamic light scattering and X-ray diffraction was used to estimate the thickness of the stabilizing layers of the polymer on the colloidal particles. Scattering of synchrotron radiation and neutrons are powerful complementary techniques to provide information about flow and the potential to apply them to systems that are beyond the scope of simple simulations has been demonstrated.
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Sekhar, Susheel Kumar. "Viscous hypersonic flow physics predictions using unstructured Cartesian grid techniques." Diss., Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/45857.

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Aerothermodynamics is an integral component in the design and implementation of hypersonic transport systems. Accurate estimates of the aerodynamic forces and heat transfer rates are critical in trajectory analysis and for payload weight considerations. The present work seeks to investigate the ability of an unstructured Cartesian grid framework in modeling hypersonic viscous flows. The effectiveness of modeling viscous phenomena in hypersonic flows using the immersed boundary ghost cell methodology of this solver is analyzed. The capacity of this framework to predict the surface physics in a hypersonic non-reacting environment is investigated. High velocity argon gas flows past a 2-D cylinder are simulated for a set of freestream conditions (Reynolds numbers), and impact of the grid cell sizes on the quality of the solution is evaluated. Additionally, the formulation is verified over a series of hypersonic Mach numbers for the flow past a hemisphere, and compared to experimental results and empirical estimates. Next, a test case that involves flow separation and the interaction between a hypersonic shock wave and a boundary layer, and a separation bubble is investigated using various adaptive mesh refinement strategies. The immersed boundary ghost cell approach is tested with two temperature clipping strategies, and their impact on the overall solution accuracy and smoothness of the surface property predictions are compared. Finally, species diffusion terms in the conservation equations, and collision cross-section based transport coefficients are installed, and hypersonic flows in thermochemical nonequilibrium environments are studied, and comparisons of the off-surface flow properties and the surface physics predictions are evaluated. First, a 2-D cylinder in a hypersonic reacting air flow is tested with an adiabatic wall boundary condition. Next, the same geometry is tested to evaluate the viscous chemistry prediction capability of the solver with an isothermal wall boundary condition, and to identify the strengths and weaknesses of the immersed boundary ghost cell methodology in computing convective heating rates in such an environment.
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Alver, Burak Han. "Measurement of non-flow correlations and elliptic flow fluctuations in Au+Au collisions at RHIC." Thesis, Massachusetts Institute of Technology, 2010. http://hdl.handle.net/1721.1/62643.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Physics, 2010.
Cataloged from PDF version of thesis.
Includes bibliographical references (p. 95-102).
Measurements of collective flow and two-particle correlations have proven to be effective tools for understanding the properties of the system produced in ultrarelativistic nucleus-nucleus collisions at the Relativistic Heavy Ion Collider (RHIC). Accurate modeling of the initial conditions of a heavy ion collision is crucial in the interpretation of these results. The anisotropic shape of the initial geometry of heavy ion collisions with finite impact parameter leads to an anisotropic particle production in the azimuthal direction through collective flow of the produced medium. In "head-on" collisions of Copper nuclei at ultrarelativistic energies, the magnitude of this "elliptic flow" has been observed to be significantly large. This is understood to be due to fluctuations in the initial geometry which leads to a significant anisotropy even for most central Cu+Cu collisions. This thesis presents a phenomenological study of the effect of initial geometry fluctuations on two-particle correlations and an experimental measurement of the magnitude of elliptic flow fluctuations which is predicted to be large if initial geometry fluctuations are present. Two-particle correlation measurements in Au+Au collisions at the top RHIC energies have shown that after correction for contributions from elliptic flow, strong azimuthal correlation signals are present at A0 = 0 and A0 ~ 120. These correlation structures may be understood in terms of event-by-event fluctuations which result in a triangular anisotropy in the initial collision geometry of heavy ion collisions, which in turn leads to a triangular anisotropy in particle production. It is observed that similar correlation structures are observed in A Multi-Phase Transport (AMPT) model and are, indeed, found to be driven by the triangular anisotropy in the initial collision geometry. Therefore "triangular flow" may be the appropriate description of these correlation structures in data. The measurement of elliptic flow fluctuations is complicated by the contributions of statistical fluctuations and other two-particle correlations (non-flow correlations) to the observed fluctuations in azimuthal particle anisotropy. New experimental techniques, which crucially rely on the uniquely large coverage of the PHOBOS detector at RHIC, are developed to quantify and correct for these contributions. Relative elliptic flow fluctuations of approximately 30-40% are observed in 6-45% most central Au+Au collisions at s NN= 200 GeV. These results are consistent with the predicted initial geometry fluctuations.
by Burak Han Alver.
Ph.D.
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Santhanakrishnan, Arvind. "CHARACTERIZATION AND FLOW PHYSICS OF PLASMA SYNTHETIC JET ACTUATORS." UKnowledge, 2007. http://uknowledge.uky.edu/gradschool_diss/545.

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Plasma synthetic jet actuators are investigated experimentally, in which the geometrical design of single dielectric barrier discharge (SDBD) plasma actuators is modified to produce zero-mass flux jets similar to those created by mechanical devices. The SDBD plasma actuator consists of two rectangular electrodes oriented asymmetrically and separated by a layer of dielectric material. Under an input of high voltage, high frequency AC or pulsed DC, a region of plasma is created in the interfacial air gap on account of electrical breakdown of the ambient air. A coupling between the electric field in the plasma and the neutral air near the actuator is introduced, such that the latter experiences a net force which results in a horizontal wall jet. This effect of the actuator has been demonstrated to be useful in mitigating boundary layer separation in aerodynamic flows. To increase the impact that a plasma actuator may have on the flow field, this research investigates the development and characterization of a novel flow control device, the plasma synthetic jet actuator, which tailors the residual air in the form of a vertical jet resembling conventional continuous and synthetic jets. This jet can be either three dimensional using annular electrode arrays, or nearly two dimensional using two rectangular strip exposed electrodes and one embedded electrode. Detailed measurements on the isolated plasma synthetic jet reveal that pulsed operation of the actuator results in the formation of multiple counterrotating vortical structures in the flow field. The output jet velocity and momentum are found to be higher for unsteady pulsing as compared to steady operation. In the case of flow over a flat plate, the actuator is observed to create a localized interaction region within which the baseline flow direction and boundary layer characteristics are modified. The efficiency of the actuator in coupling momentum to the neutral air is found to be related to the plasma morphology, pulsing frequency, actuator dimension, and input power. An analytical scaling model is proposed to describe the effects of varying the above variables on the output jet characteristics and actuator efficiency, and the experimental data is used for model validation.
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Freed, David M. (David Michael). "A digital physics method for two phase flow." Thesis, Massachusetts Institute of Technology, 1997. http://hdl.handle.net/1721.1/43571.

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Chinn, John Joss. "The internal flow physics of swirl atomizer nozzles." Thesis, University of Manchester, 1996. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.488302.

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The internal flow of pressure swirl atomizers is studied with the ultimate aim of developing a design tool for such atomizers, particularly to enable the production of the finest possible water sprays (for any given supply pressure) for fire suppression purposes. The primary direction of the research was in computationally modelling this flow with a two-dimensional assumption and a methodology is described which is capable of determining the velocity profiles and, for the first time in the literature, the air-core topology and discharge coefficient, for nozzles which approximate the axially-symmetric condition. The results are compared with the experimental results from both the literature and also from research which was carried out under the supervision of the author. The predictions show important flow features, which are found in the experiments and have not been recognised in the "classically" assumed internal flow. These include concentration of the axial flow near the air-core and toroidal vortices, similar to Taylor-Göertler vortices found in Taylor-Couette flow, which are visible in planes through the nozzle axis. The secondary direction of the research is in both reviewing and improving upon simplified analytical techniques which have been used to estimate the size of the air-core radius at the nozzle exit together with the values of the discharge coefficient and the cone angle of the resultant spray. A critical review is given of many of the existing analytical techniques and a new analytical theory is presented which is based upon a balance of the axial momentum across a control volume. The results of the new theory are compared with the experimental findings reported in the literature and show the need to include the swirl chamber/nozzle orifice ratio as an independent variable. Suggestions are given on how the computational methodology might be employed to determine the spray drop size for a given atomizer design and on the direction the computational work might take in order to predict a full two-phase internal flow using volume of fluid (VOF) techniques.
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Books on the topic "Physics of flow"

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Zamir, M. The Physics of Pulsatile Flow. New York, NY: Springer New York, 2000.

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The physics of pulsatile flow. New York: AIP Press, 2000.

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Zamir, M. The Physics of Pulsatile Flow. New York, NY: Springer New York, 2000. http://dx.doi.org/10.1007/978-1-4612-1282-9.

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Barnwell, R. W. Natural Laminar Flow and Laminar Flow Control. New York, NY: Springer New York, 1992.

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Jou, David. Thermodynamics of Fluids Under Flow. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001.

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Durão, D. F. G. Combustings Flow Diagnostics. Dordrecht: Springer Netherlands, 1992.

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Schobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. 2nd ed. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.

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Turbomachinery flow physics and dynamic performance. Berlin: Springer, 2005.

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Schobeiri, Meinhard. Turbomachinery flow physics and dynamic performance. 2nd ed. New York: Springer, 2012.

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Zamir, M. The physics of coronary blood flow. New York: Springer, 2005.

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Book chapters on the topic "Physics of flow"

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Hu, Wenbing. "Polymer Flow." In Polymer Physics, 127–44. Vienna: Springer Vienna, 2012. http://dx.doi.org/10.1007/978-3-7091-0670-9_7.

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Hsü, Kenneth J. "Suspensions Flow." In Physics of Sedimentology, 89–101. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-09296-5_6.

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Nichols, Daniel H. "Fluid Flow." In Physics for Technology, 151–66. Second edition. | Boca Raton : CRC Press, Taylor & Francis: CRC Press, 2018. http://dx.doi.org/10.1201/9781351207270-9.

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Malkin, A. Ya, and P. V. Zhirkov. "Flow of polymerizing liquids." In Polymer Physics, 111–47. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/3-540-52159-3_7.

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Livan, Michele, and Richard Wigmans. "Particle Flow Analysis." In UNITEXT for Physics, 245–56. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-23653-3_12.

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McCormack, Percival. "Nanoduct Fluid Flow." In SpringerBriefs in Physics, 119–36. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4614-0257-2_4.

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Feldmeier, Achim. "Vortices, Corner Flow, and Flow Past Plates." In Theoretical and Mathematical Physics, 115–60. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-31022-6_4.

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Hahn, George M. "Blood Flow." In Physics and Technology of Hyperthermia, 441–47. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3597-6_19.

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Arthur, Richard T. W. "Classical Physics and Becoming." In The Reality of Time Flow, 69–107. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-15948-1_4.

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Khoshyaran, Megan M., and Jean-Patrick Lebacque. "Continuum Traffic Flow Modelling: Network Approximation, Flow Approximation." In Springer Proceedings in Physics, 505–13. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-55973-1_62.

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Conference papers on the topic "Physics of flow"

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WEINSTEIN, L., G. BEELER, and A. LINDEMANN. "High-speed holocinematographic velocimeter for studying turbulent flow control physics." In Shear Flow Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-526.

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Pidugu, S. B., and T. Bayraktar. "Flow Physics in Microchannels." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-80561.

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Even though microfluidic devices are slowly becoming commercial reality (e.g. Inkjet printers), the challenges in the design of microfluidic devices remain since not all aspects of fluid flow in microchannels have been fully understood yet. This paper presents an extensive review of studies on flow physics for both pressure-driven and electrokinetic flows in microchannels. The primary goal of the present paper is to provide a wide overview of findings on underlying principles of microflow physics. The issues discussed include the effect of pressure drop and friction measurements; mixing and flow control methods for microfluidic systems; and joule heating and viscous dissipation effects in microchannel flows. No agreement has been found among studies focusing on the characterization of friction factor/pressure drop for microflow systems. Further investigation requires understanding how entrance effects differ in the case of microflows when compared to macro scale flow. There is a clear need to investigate characteristics of non-Newtonian fluid flow in microchannels.
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Lindstrom, Annika, Marianne Monastero, and Michael Amitay. "The Flow Physics of Synthetic Jets Interaction with Flow over a Flapped Airfoil." In 2018 Flow Control Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4019.

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Kogan, M. N., and A. A. Basalaev. "Investigation of cross flow forces influence on incompressible laminar flow." In Progress in Flight Physics. Les Ulis, France: EDP Sciences, 2012. http://dx.doi.org/10.1051/eucass/201203513.

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Liu, Tianshu, Bo Wang, Bo Wang, and S. Woodiga. "Physics-Based Optical Flow Method in Global Flow Diagnostics." In 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4361.

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Tang, A. H. "Flow and non-flow correlations from four-particle multiplets in STAR." In NUCLEAR PHYSICS IN THE 21st CENTURY:International Nuclear Physics Conference INPC 2001. AIP, 2002. http://dx.doi.org/10.1063/1.1469992.

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Werner, Klaus. "Flow in proton-nucleus collisions." In The European Physical Society Conference on High Energy Physics. Trieste, Italy: Sissa Medialab, 2014. http://dx.doi.org/10.22323/1.180.0201.

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Knight, D. "A summary of laser and microwave flow control in high-speed flows." In Progress in Flight Physics, edited by P. Reijasse, D. Knight, M. Ivanov, and I. Lipatov. Les Ulis, France: EDP Sciences, 2013. http://dx.doi.org/10.1051/eucass/201305125.

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Shannon, Daniel, Scott Morris, and Thomas Mueller. "Trailing Edge Flow Physics and Acoustics." In 11th AIAA/CEAS Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-2957.

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Sikivie, Pierre. "The Big Flow." In COSMOLOGY AND ELEMENTARY PARTICLE PHYSICS: Coral Gables Conference on Cosmology and Elementary Particle Physics. AIP, 2002. http://dx.doi.org/10.1063/1.1492155.

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Reports on the topic "Physics of flow"

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Tan, Choon S. Aerospace Turbomachinery Flow Physics. Fort Belvoir, VA: Defense Technical Information Center, August 2003. http://dx.doi.org/10.21236/ada418327.

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Ukeiley, Lawrence, and Louis Cattafesta. On the Flow Physics of Effectively Controlled Open Cavity Flows. Fort Belvoir, VA: Defense Technical Information Center, May 2013. http://dx.doi.org/10.21236/ada584446.

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Knight, Doyle, Hong Yan, Greg Elliott, Nick Glumac, Graham Candler, and Alexander Zheltovodov. Fundamental Physics and Practical Applications of Electromagnetic Local Flow Control in High Speed Flows. Fort Belvoir, VA: Defense Technical Information Center, February 2007. http://dx.doi.org/10.21236/ada466943.

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Candler, Graham V. Fundamental Physics and Practical Applications of Electromagnetic Local Flow Control in High Speed Flows. Fort Belvoir, VA: Defense Technical Information Center, April 2010. http://dx.doi.org/10.21236/ada588544.

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Tian, Ye, III Cattafesta, and Louis N. Separation Control Using ZNMF Devices: Flow Physics and Scaling Laws. Fort Belvoir, VA: Defense Technical Information Center, December 2007. http://dx.doi.org/10.21236/ada481565.

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Hess, Mark, and Evstati Evstatiev. Effects of Radiation Reaction Physics on High-Current Power Flow. Office of Scientific and Technical Information (OSTI), August 2021. http://dx.doi.org/10.2172/1814239.

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Juanes, Ruben. Nonequilibrium Physics and Phase-Field Modeling of Multiphase Flow in Porous Media. Office of Scientific and Technical Information (OSTI), September 2016. http://dx.doi.org/10.2172/1332323.

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Santarius, John F., and Gilbert A. Emmert. Atomic Physics Effects on Convergent, Child-Langmuir Ion Flow between Nearly Transparent Electrodes. Office of Scientific and Technical Information (OSTI), November 2013. http://dx.doi.org/10.2172/1104537.

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Brennan, Dylan P. Flow Shear Effects in the Onset Physics of Resistive MHD Instabilities in Tokamaks. Final report. Office of Scientific and Technical Information (OSTI), April 2013. http://dx.doi.org/10.2172/1093495.

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Moore, Murray E. Define and Quantify the Physics of Air Flow, Pressure Drop and Aerosol Collection in Nuclear Grade HEPA Filters. Office of Scientific and Technical Information (OSTI), February 2015. http://dx.doi.org/10.2172/1170705.

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