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1

Sonnenberger, R. J., C. N. Nayeri, H. H. Fernholz, and C. O. Paschereit. "Active control of the separated flow behind a fence(Flow Control 1)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 375–77. http://dx.doi.org/10.1299/jsmeicjwsf.2005.375.

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2

FFOWCS WILLIAMS, J. E. "ACTIVE FLOW CONTROL." Journal of Sound and Vibration 239, no. 4 (2001): 861–71. http://dx.doi.org/10.1006/jsvi.2000.3225.

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3

Toroczkai, Zoltán, and Tamás Tél. "Introduction: Active chaotic flow." Chaos: An Interdisciplinary Journal of Nonlinear Science 12, no. 2 (2002): 372. http://dx.doi.org/10.1063/1.1482195.

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4

Arad, Eran, Manikandan Ramasamy, and Jacob S. Wilson. "Flow Response of Active Flow Control Actuators." AIAA Journal 52, no. 5 (2014): 998–1009. http://dx.doi.org/10.2514/1.j052419.

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5

YAMAMOTO, Hideaki, Noriyuki NAKANO, Masahiro WATANABE, and Kensuke HARA. "2D21 Active Feedback Control of a Leakage-Flow-Induced Vibration of Translational 1DOF System by Flow Control." Proceedings of the Symposium on the Motion and Vibration Control 2010 (2010): _2D21–1_—_2D21–16_. http://dx.doi.org/10.1299/jsmemovic.2010._2d21-1_.

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6

Dearing, S., S. Lambert, and J. Morrison. "Flow control with active dimples." Aeronautical Journal 111, no. 1125 (2007): 705–14. http://dx.doi.org/10.1017/s0001924000004887.

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Abstract The long-term goal is to design and manufacture optimal ‘on-demand’ vortex generators, ‘dimples’ that can produce vortices of prescribed strength and duration for the real-time control of aerodynamic flows that are either undergoing transition or are fully turbulent, attached or separating. Electro-active polymers (EAP) are ideal for a dimple control surface, offering high strain rate, fast response, and high electromechanical efficiency. EAP can also be used as the basis of a resistanc – or capacitance – change pressure sensor, development of which has just begun. In terms of manufac
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7

Cattafesta, Louis N., and Mark Sheplak. "Actuators for Active Flow Control." Annual Review of Fluid Mechanics 43, no. 1 (2011): 247–72. http://dx.doi.org/10.1146/annurev-fluid-122109-160634.

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8

Woodhouse, Francis G., Aden Forrow, Joanna B. Fawcett, and Jörn Dunkel. "Stochastic cycle selection in active flow networks." Proceedings of the National Academy of Sciences 113, no. 29 (2016): 8200–8205. http://dx.doi.org/10.1073/pnas.1603351113.

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Active biological flow networks pervade nature and span a wide range of scales, from arterial blood vessels and bronchial mucus transport in humans to bacterial flow through porous media or plasmodial shuttle streaming in slime molds. Despite their ubiquity, little is known about the self-organization principles that govern flow statistics in such nonequilibrium networks. Here we connect concepts from lattice field theory, graph theory, and transition rate theory to understand how topology controls dynamics in a generic model for actively driven flow on a network. Our combined theoretical and
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9

Khomich, Vladislav Yu, and Vladimir A. Yamshchikov. "Electrohydrodynamic flow for the active control of gas flows." Uspekhi Fizicheskih Nauk 187, no. 06 (2017): 653–66. http://dx.doi.org/10.3367/ufnr.2017.01.038047.

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10

Khomich, V. Yu, and V. A. Yamshchikov. "Electrohydrodynamic flow for the active control of gas flows." Physics-Uspekhi 60, no. 6 (2017): 608–20. http://dx.doi.org/10.3367/ufne.2017.01.038047.

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11

Shanan, Yahya Hamza. "Active flow control of a diffusing S-duct." International Journal of Engineering, Science and Technology 12, no. 2 (2020): 1–10. http://dx.doi.org/10.4314/ijest.v12i2.1.

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Realization of the S-duct benefits requires scrutiny of certain phenomena such as swirls, secondary flows, and flow distortion creation which are related to the S-duct due to its physical curvature. The first phase of the study investigated the flow field inside the S-duct. NASA Glenn research center’s S-duct was adopted in this study. Geometry was created in SOLIDWORKS and mesh was done using ICEM CFD. Numerical analysis was carried out in ANSYS Fluent software. A turbulence model named kω-SST was incorporated. Boundary conditions were set so as to match the experimental test done by NASA Gle
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12

Poltronieri Sampaio, Leonardo, Moacyr Aureliano Gomes de Brito, Guilherme de Azevedo e Melo, and Carlos Alberto Canesin. "Grid-tie Three-phase Inverter With Active And Reactive Power Flow Control Capability." Eletrônica de Potência 19, no. 4 (2014): 397–405. http://dx.doi.org/10.18618/rep.2014.4.397405.

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13

HASEGAWA, Hiroaki, Yukihiro SAWADA, and Kazuo MATSUUCHI. "ACTIVE SEPARATION CONTROL USING VORTEX GENERATOR JETS WITH TRIANGULAR ORIFICES(Flow Control 1)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 363–68. http://dx.doi.org/10.1299/jsmeicjwsf.2005.363.

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14

Takehiko, Segawa, and Matsunuma Takayuki. "IL10 ACTIVE FLOW CONTROL ON TURBINE BLADES BY DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATORS." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _IL10–1_—_IL10–10_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._il10-1_.

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15

Gao, Chuanqiang, Weiwei Zhang, Jiaqing Kou, Yilang Liu, and Zhengyin Ye. "Active control of transonic buffet flow." Journal of Fluid Mechanics 824 (July 5, 2017): 312–51. http://dx.doi.org/10.1017/jfm.2017.344.

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Transonic buffet is a phenomenon of aerodynamic instability with shock wave motions which occurs at certain combinations of Mach number and mean angle of attack, and which limits the aircraft flight envelope. The objective of this study is to develop a modelling method for unstable flow with oscillating shock waves and moving boundaries, and to perform model-based feedback control of the two-dimensional buffet flow by means of trailing-edge flap oscillations. System identification based on the ARX algorithm is first used to derive a linear model of the input–output dynamics between the flap ro
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16

Strunin, Dmitry. "Fluid flow between active elastic plates." ANZIAM Journal 50 (May 23, 2009): 871. http://dx.doi.org/10.21914/anziamj.v50i0.1452.

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17

Popović, Marko, Amitabha Nandi, Matthias Merkel, et al. "Active dynamics of tissue shear flow." New Journal of Physics 19, no. 3 (2017): 033006. http://dx.doi.org/10.1088/1367-2630/aa5756.

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18

Gudmundsson, Agust. "Active fault zones and groundwater flow." Geophysical Research Letters 27, no. 18 (2000): 2993–96. http://dx.doi.org/10.1029/1999gl011266.

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19

Alfredsson, K. S. "Active and Reactive Structural Energy Flow." Journal of Vibration and Acoustics 119, no. 1 (1997): 70–79. http://dx.doi.org/10.1115/1.2889689.

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Vibration of linear structures having internal material damping is considered. Energy supplied to such structures by external dynamic loads and mechanical energy flow inside these structures are investigated. The paper aims at presenting and discussing relations which are useful when studying energy transmission through mechanical systems. Special attention is paid to the case of stationary harmonic vibration, but general stationary vibration is also discussed. Continuity equations for the active and reactive mechanical intensities are derived for a solid continuum model. Limits for the active
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20

Singh, Deepesh Kumar, and Gautam Bandyopadhyay. "Active Flow Control over the Car." Applied Mechanics and Materials 110-116 (October 2011): 2521–28. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.2521.

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Active flow control methods are used to reduce the aerodynamic drag over a car model. Method of Boundary layer suction at the top rear and air injection at the back of the car are used as the active flow control tools to suppress the aerodynamic drag. The computational results obtained using the standard model for the car model are verified first against the practical results obtained by wind tunnel experimentation so as to obtain the range of turbulence. Then a parametric study on the effect of the drag and lift coefficient of the car with respect to the parameters governing the active flow c
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21

Venkatraman, K., and S. Narayanan. "Active Control Of Flow-induced Vibration." Journal of Sound and Vibration 162, no. 1 (1993): 43–55. http://dx.doi.org/10.1006/jsvi.1993.1101.

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22

Gao, Na, Chen Pu, and Bao Chen. "Accuracy Investigation of Active Flow Control Using Synthetic Jets." Applied Mechanics and Materials 741 (March 2015): 475–80. http://dx.doi.org/10.4028/www.scientific.net/amm.741.475.

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2nd order implicit format is implemented in the Navier-Stokes code to deal with instantaneous item unsteady flows. Three simulations are made to testify the method on flow control. First, the external flow fields of synthetic jets are simulated, the mean velocity on the center line, the jet width and velocity distribution are compared well with experimental results. Secondly, the flow fields of synthetic jet in a crossflow are simulated, orifice slot, the mean velocity on the center line and velocity distribution are compared well with experimental results. Finally, the flow control experiment
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23

Wang, Weiqiang, and Rui Zhang. "Interplay of Active Stress and Driven Flow in Self-Assembled, Tumbling Active Nematics." Crystals 11, no. 9 (2021): 1071. http://dx.doi.org/10.3390/cryst11091071.

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Lyotropic chromonic liquid crystals (LCLCs) are a special type of hierarchical material in which self-assembled molecular aggregates are responsible for the formation of liquid crystal phases. Thanks to its unusual material properties and bio compatibility, it has found wide applications including the formation of active nematic liquid crystals. Recent experiments have uncovered tumbling character of certain LCLCs. However, how tumbling behavior modifies structure and flow in driven and active nematics is poorly understood. Here, we rely on continuum simulation to study the interplay of extens
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24

Oo, Thandar, Su Mon Myint, and Aye Khaing Zin. "Analysis of Active Power Flow Control with Phase Shifting Transformer in AC Transmission Line." International Journal of Trend in Scientific Research and Development Volume-2, Issue-6 (2018): 666–72. http://dx.doi.org/10.31142/ijtsrd18593.

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25

Paschereit, C. O., and B. Schuermans. "Combustion instability suppression by active control of the burner mixing profile(Flow Control 1)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 369–74. http://dx.doi.org/10.1299/jsmeicjwsf.2005.369.

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26

Bae, Jin Woo, Kenneth S. Breuer, and Choon S. Tan. "Active Control of Tip Clearance Flow in Axial Compressors." Journal of Turbomachinery 127, no. 2 (2005): 352–62. http://dx.doi.org/10.1115/1.1776584.

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Control of compressor tip clearance flows is explored in a linear cascade using three types of fluidic actuators; normal synthetic jet (NSJ; unsteady jet normal to the mean flow with zero net mass flux), directed synthetic jet (DSJ; injection roughly aligned with the mean flow), and steady directed jet (SDJ), mounted on the casing wall. The effectiveness of each active control technique is determined in terms of its ability to achieve: (1) reduction of tip leakage flow rate, (2) mixing enhancement between tip leakage and core flow, and (3) increase in streamwise momentum of the flow in the end
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27

Manoj Kumar, Vedulla, and Chin-Cheng Wang. "Active Flow Control of Flapping Airfoil Using Openfoam." Journal of Mechanics 36, no. 3 (2019): 361–72. http://dx.doi.org/10.1017/jmech.2019.46.

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ABSTRACTThe concept of the fixed wing Micro Air Vehicles (MAVs) has received increasing interest over the past few decades, with the principal aim of carrying out the surveillance missions. The design of the flapping wing MAVs still is in infancy stage. On the other hand, there has been increasing interest over the flow control using plasma actuators in worldwide. The aim of this research is to study the flow control of a flapping airfoil with and without plasma actuation in OpenFOAM. The OpenFOAM CFD platform has been used to develop our own plasma solver. For the plasma induced turbulence in
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28

Caillaud, Se´bastien, Emmanuel de Langre, and Franck Baj. "Active Vibration Control for the Measurement of Fluidelastic Effects." Journal of Pressure Vessel Technology 125, no. 2 (2003): 165–70. http://dx.doi.org/10.1115/1.1561451.

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A new method based on active vibration control is proposed to investigate fluidelastic coupling effects beyond fluidelastic instability. This active control method allows to extend the range of flow velocity explored for single input-single output control systems. The method is applied on a flexible tube inserted in a rigid bundle in water and air-water cross-flows. This structure becomes unstable for high flow velocities, fluidelastic forces then causing the damping of the fluid-structure system to fall towards zero. The active control method allows to carry out tests beyond the fluidelastic
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29

Miyagi, Norimasa, Kohei Hodoya, Hajime Fujita, Hideo Shoji, and Motoaki Kimura. "Study of Active Jet Control by Acoustically driven Secondary Film Flow : Influence of Velocity Ratio and Acoustic Strouhal Number(Flow Control 2)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 459–64. http://dx.doi.org/10.1299/jsmeicjwsf.2005.459.

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30

Strecker, H., and N. Bello González. "Evolution of the flow field in decaying active regions." Astronomy & Astrophysics 620 (December 2018): A122. http://dx.doi.org/10.1051/0004-6361/201732164.

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Context. Fully fledged sunspots are known to be surrounded by a radial outflow called the moat flow. Aims. We investigate the evolution of the horizontal flow field around sunspots during their decay, that is, from fully fledged to naked spots, after they loose the penumbra, to the remnant region after the spot has fully dissolved. Methods. We analysed the extension and horizontal velocity of the flow field around eight sunspots using SDO/HMI Doppler maps. By assuming a radially symmetrical flow field, the applied analysis method determines the radial dependence of the azimuthally averaged flo
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31

Kang, Hyun-Myoung, Hoan-Suk Choi, and Woo-Seop Rhee. "QoS Adaptive Flow based Active Queue Management Algorithm and Performance Analysis." Journal of the Korea Contents Association 10, no. 3 (2010): 80–91. http://dx.doi.org/10.5392/jkca.2010.10.3.080.

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32

Olwi, Ibrahim. "Experimental Investigation of the Flow Field Characteristics under Active Flow Control." International Journal of Fluid Mechanics Research 41, no. 2 (2014): 169–83. http://dx.doi.org/10.1615/interjfluidmechres.v41.i2.50.

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33

Mushyam, Aditya, and Josep M. Bergada. "Active Flow Control on Laminar flow over a Backward facing step." Journal of Physics: Conference Series 633 (September 21, 2015): 012110. http://dx.doi.org/10.1088/1742-6596/633/1/012110.

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34

Simon, B., T. Nemitz, J. Rohlfing, F. Fischer, D. Mayer, and S. Grundmann. "Active flow control of laminar boundary layers for variable flow conditions." International Journal of Heat and Fluid Flow 56 (December 2015): 344–54. http://dx.doi.org/10.1016/j.ijheatfluidflow.2015.09.003.

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35

Wang, Liang, Ruyun Hu, Liying Li, and Song Fu. "Detached-Eddy Simulations for Active Flow Control." AIAA Journal 56, no. 4 (2018): 1447–62. http://dx.doi.org/10.2514/1.j055891.

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36

Bons, Jeffrey, Stuart Benton, Chiara Bernardini, and Matthew Bloxham. "Active Flow Control for Low-Pressure Turbines." AIAA Journal 56, no. 7 (2018): 2687–98. http://dx.doi.org/10.2514/1.j056697.

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37

Andino, Marlyn Y., John C. Lin, Seele Roman, et al. "Active Flow Control on Vertical Tail Models." AIAA Journal 57, no. 8 (2019): 3322–38. http://dx.doi.org/10.2514/1.j057876.

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38

Martín-Gómez, Aitor, Gerhard Gompper, and Roland Winkler. "Active Brownian Filamentous Polymers under Shear Flow." Polymers 10, no. 8 (2018): 837. http://dx.doi.org/10.3390/polym10080837.

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The conformational and rheological properties of active filaments/polymers exposed to shear flow are studied analytically. Using the continuous Gaussian semiflexible polymer model extended by the activity, we derive analytical expressions for the dependence of the deformation, orientation, relaxation times, and viscosity on the persistence length, shear rate, and activity. The model yields a Weissenberg-number dependent shear-induced deformation, alignment, and shear thinning behavior, similarly to the passive counterpart. Thereby, the model shows an intimate coupling between activity and shea
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39

Cattafesta, Louis N., Qi Song, David R. Williams, Clarence W. Rowley, and Farrukh S. Alvi. "Active control of flow-induced cavity oscillations." Progress in Aerospace Sciences 44, no. 7-8 (2008): 479–502. http://dx.doi.org/10.1016/j.paerosci.2008.07.002.

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40

Ferlin, Francesco, Daniela Lanari, and Luigi Vaccaro. "Sustainable flow approaches to active pharmaceutical ingredients." Green Chemistry 22, no. 18 (2020): 5937–55. http://dx.doi.org/10.1039/d0gc02404j.

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This review summarizes the adoption of flow technology for the synthesis of a variety of APIs in the period 2015–2020. A major attention has been dedicated to compare batch and flow procedures by also comparing their sustainability.
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41

Lauchle, Gerald C., John R. MacGillivray, and David C. Swanson. "Active control of axial-flow fan noise." Journal of the Acoustical Society of America 101, no. 1 (1997): 341–49. http://dx.doi.org/10.1121/1.417979.

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42

Wang, Wei, Spiridon Siouris, and Ning Qin. "Hybrid RANS/LES for active flow control." Aircraft Engineering and Aerospace Technology 86, no. 3 (2014): 179–87. http://dx.doi.org/10.1108/aeat-01-2013-0012.

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43

Bieler, Heribert. "Active flow control concepts and application opportunities." Aircraft Engineering and Aerospace Technology 89, no. 5 (2017): 725–29. http://dx.doi.org/10.1108/aeat-01-2017-0015.

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Purpose Aerodynamics drives the aircraft performance and, thus, influences fuel consumption and environmental compatibility. Further, optimization of aerodynamic shapes is an ongoing design activity in industrial offices; this will lead to incremental improvements. More significant step changes in performance are not expected from pure passive shape design. However, active flow control is a key technology, which has the potential to realize a drastic step change in performance. Flow control targets two major goals: low speed performance enhancements mainly for start and landing phase via contr
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44

Louis, Sarah, Elco Luijendijk, István Dunkl, and Mark Person. "Episodic fluid flow in an active fault." Geology 47, no. 10 (2019): 938–42. http://dx.doi.org/10.1130/g46254.1.

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Abstract We present a reconstruction of episodic fluid flow over the past ∼250 k.y. along the Malpais normal fault, which hosts the Beowawe hydrothermal system (Nevada, USA), using a novel combination of the apatite (U-Th)/He (AHe) thermochronometer and a model of the thermal effects of fluid flow. Samples show partial resetting of the AHe thermochronometer in a 40-m-wide zone around the fault. Numerical models using current fluid temperatures and discharge rates indicate that fluid flow events lasting 2 k.y. or more lead to fully reset samples. Episodic fluid pulses lasting 1 k.y. result in p
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45

Olivier, Ducloux, Talbi Abdelkrim, Deblock Yves, et al. "Magnetically actuated microvalve for active flow control." Journal of Physics: Conference Series 34 (April 1, 2006): 631–36. http://dx.doi.org/10.1088/1742-6596/34/1/104.

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46

Paragios, N., O. Mellina-Gottardo, and V. Ramesh. "Gradient vector flow fast geometric active contours." IEEE Transactions on Pattern Analysis and Machine Intelligence 26, no. 3 (2004): 402–7. http://dx.doi.org/10.1109/tpami.2004.1262337.

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47

MacGillivray, John R., Gerald C. Lauchle, and David C. Swanson. "Active control of axial‐flow fan noise." Journal of the Acoustical Society of America 98, no. 5 (1995): 2885. http://dx.doi.org/10.1121/1.413142.

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48

Rumsey, C. L., and R. C. Swanson. "Turbulence modelling for active flow control applications." International Journal of Computational Fluid Dynamics 23, no. 4 (2009): 317–26. http://dx.doi.org/10.1080/10618560902776794.

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49

Aweya, James, Michel Ouellette, and Delfin Y. Montuno. "Active queue management with flow proportional buffering." International Journal of Network Management 13, no. 3 (2003): 211–29. http://dx.doi.org/10.1002/nem.479.

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50

Voituriez, R., J. F. Joanny, and J. Prost. "Spontaneous flow transition in active polar gels." Europhysics Letters (EPL) 70, no. 3 (2005): 404–10. http://dx.doi.org/10.1209/epl/i2004-10501-2.

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