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Journal articles on the topic 'Control flow separation'

Author: Grafiati

Published: 28 May 2022

Last updated: 31 July 2025

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1

Lu, Weiyu, Guoping Huang, Jinchun Wang, and Yuxuan Yang. "Interpretation of Four Unique Phenomena and the Mechanism in Unsteady Flow Separation Controls." Energies 12, no. 4 (2019): 587. http://dx.doi.org/10.3390/en12040587.

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Unsteady flow separation controls are effective in suppressing flow separations. However, the unique phenomena in unsteady separation control, including frequency-dependent, threshold, location-dependent, and lock-on effects, are not fully understood. Furthermore, the mechanism of the effectiveness that lies in unsteady flow controls remains unclear. Thus, this study aims to interpret further the unique phenomena and mechanism in unsteady flow separation controls. First, numerical simulation and some experimental results of a separated curved diffuser using pulsed jet flow control are discusse

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2

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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3

Gad-el-Hak, Mohamed, and Dennis M. Bushnell. "Separation Control: Review." Journal of Fluids Engineering 113, no. 1 (1991): 5–30. http://dx.doi.org/10.1115/1.2926497.

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Under certain conditions, wall-bounded flows separate. To improve the performance of natural or man-made flow systems, it may be beneficial to delay or advance this detachment process. The present article reviews the status and outlook of separation control for both steady and unsteady flows. Both passive and active techniques to prevent or to provoke flow detachment are considered and suggestions are made for further research.

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4

Arifuzzaman, Md. "Flow Separation Control on Flapped Airfoil." IOSR Journal of Engineering 02, no. 07 (2012): 137–40. http://dx.doi.org/10.9790/3021-0271137140.

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5

Vaisakh, S., and TM Muruganandam. "Influence of multi-wall separation control on normal-shock-induced separation in supersonic duct flows." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 9 (2018): 3184–92. http://dx.doi.org/10.1177/0954410018793789.

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In this work, separation due to the interaction of normal shock with wall boundary layers in a supersonic duct flow is studied using schlieren, oil flow visualization, and pressure measurements. This study uses separation control devices on three walls of a rectangular duct and investigates the influence of adding control on one wall and on the other walls. It was found that control on any wall has effect on separation on other walls. This effect was found to be due to the change in the size of corner separations. Pressure recovery was found to be steeper with the introduction of more control

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6

Segawa, Takehiko, Daiki Suzuki, Takayasu Fujino, Timothy Jukes, and Takayuki Matsunuma. "Feedback Control of Flow Separation Using Plasma Actuator and FBG Sensor." International Journal of Aerospace Engineering 2016 (2016): 1–16. http://dx.doi.org/10.1155/2016/8648919.

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A feedback control system for mitigating flow separation was developed by using a string-type dielectric-barrier-discharge (DBD) plasma actuator and a fiber Bragg grating (FBG) sensor. Tangential jets were induced from the string-type DBD plasma actuator, which was located at 5% chord from the leading edge of an NACA0024 airfoil. The FBG sensor was attached to the interior surface near the root of the cantilever beam modeled on the pressure surface of the airfoil. The strain at the cantilever root was reflected in the form of Bragg wavelengths (λB) detected by the FBG sensor when the cantileve

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7

Kozo, Fujii. "IL03 RECENT FINDINGS ON THE MECHANISM OF FLOW SEPARATION CONTROL BY MICRO DEVICES." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _IL03–1_—_IL03–4_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._il03-1_.

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8

Gad-el-Hak, Mohamad. "Flow Control." Applied Mechanics Reviews 42, no. 10 (1989): 261–93. http://dx.doi.org/10.1115/1.3152376.

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The ability to actively or passively manipulate a flow field to effect a desired change is of immense technological importance. In this article, methods of control to achieve transition delay, separation postponement, lift enhancement, drag reduction, turbulence augmentation, or noise suppression are considered. The treatment is tutorial at times, making the material accessible to the advanced graduate student in the field of fluid mechanics. Emphasis is placed on external boundary-layer flows although applicability of some of the methods reviewed for internal flows will be mentioned. An attem

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9

Lang, Amy, Philip Motta, Maria Laura Habegger, Robert Hueter, and Farhana Afroz. "Shark Skin Separation Control Mechanisms." Marine Technology Society Journal 45, no. 4 (2011): 208–15. http://dx.doi.org/10.4031/mtsj.45.4.12.

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AbstractDrag reduction by marine organisms has undergone millions of years of natural selection, and from these organisms biomimetic studies can derive new technologies. The shortfin mako (Isurus oxyrinchus), considered to be one of the fastest and most agile marine predators, is known to have highly flexible scales on certain locations of its body. This scale flexibility is theorized to provide a passive, flow-actuated mechanism for controlling flow separation and thereby decreasing drag. Recent biological observations have found that the shortfin mako has highly flexible scales, bristling to

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10

Luo, Shichao, Jun Liu, Hao Jiang, and Junyuan Wang. "Magnetohydrodynamic Control of Hypersonic Separation Flows." International Journal of Aerospace Engineering 2021 (January 13, 2021): 1–13. http://dx.doi.org/10.1155/2021/6652795.

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Magnetohydrodynamic (MHD) control of hypersonic laminar separation flows is investigated in this paper. A series of numerical simulations over various geometry configurations, namely, a compression corner and a double wedge ramp hypersonic inlet, have been conducted by application of an external electromagnetic field. Results show that the performance of MHD separation flow control is mainly determined by flow acceleration of the Lorentz force directed in the streamwise direction. The Joule heating term always brings negative effects on the MHD separation flow control and increased the static

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11

Löffler, Stephan, Carola Ebert, and Julien Weiss. "Fluidic-Oscillator-Based Pulsed Jet Actuators for Flow Separation Control." Fluids 6, no. 4 (2021): 166. http://dx.doi.org/10.3390/fluids6040166.

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The control of flow separation on aerodynamic surfaces remains a fundamental goal for future air transportation. On airplane wings and control surfaces, the effects of flow separation include decreased lift, increased drag, and enhanced flow unsteadiness and noise, all of which are detrimental to flight performance, fuel consumption, and environmental emissions. Many types of actuators have been designed in the past to counter the negative effects of flow separation, from passive vortex generators to active methods like synthetic jets, plasma actuators, or sweeping jets. At the Chair of Aerody

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12

Zhang, Yingjie, Yanfeng Zhang, Xingen Lu, Ge Han, and Ziliang li. "Effects of a slotted diffuser on the aerodynamic performance of a highly loaded centrifugal compressor." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 233, no. 19-20 (2019): 6879–91. http://dx.doi.org/10.1177/0954406219865921.

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High-pressure ratio centrifugal compressors usually adopt vaned diffusers to reach high efficiency. Nevertheless, the compressor operating range might be narrow on account of the diffuser stall resulting from the large flow separations in diffuser passages at low flow rates. Flow control techniques, aimed at expanding the compressor operating range, are required to suppress these flow separations. In this paper, the flow control strategy, in terms of the slotted diffuser was used to widen the operating range for a highly loaded centrifugal compressor. The main focus of the research is to addre

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13

Abdel-Fattah, A. "Control of Separation Flow in Sudden Enlargement." International Journal of Fluid Mechanics Research 38, no. 2 (2011): 122–43. http://dx.doi.org/10.1615/interjfluidmechres.v38.i2.30.

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14

Kara, Kursat, Daegyoum Kim, and Philip J. Morris. "Flow-Separation Control Using Sweeping Jet Actuator." AIAA Journal 56, no. 11 (2018): 4604–13. http://dx.doi.org/10.2514/1.j056715.

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15

Abdel- Fattah, A. "CONTROL OF SEPARATION FLOW IN SUDDEN ENLARGEMENT." ERJ. Engineering Research Journal 33, no. 3 (2010): 251–63. http://dx.doi.org/10.21608/erjm.2010.67327.

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16

Sinha, Sumon K. "Flow Separation Control with Microflexural Wall Vibrations." Journal of Aircraft 38, no. 3 (2001): 496–503. http://dx.doi.org/10.2514/2.2789.

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17

Nishioka, M., M. Asai, and S. Yoshida. "Control of flow separation by acoustic excitation." AIAA Journal 28, no. 11 (1990): 1909–15. http://dx.doi.org/10.2514/3.10498.

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18

Seyedashraf, Omid, and Ali Akbar Akhtari. "Flow separation control in open-channel bends." Journal of the Chinese Institute of Engineers 39, no. 1 (2015): 40–48. http://dx.doi.org/10.1080/02533839.2015.1066942.

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19

Riley, N. "On the control of laminar flow separation." Quarterly Journal of Mechanics and Applied Mathematics 57, no. 2 (2004): 237–44. http://dx.doi.org/10.1093/qjmam/57.2.237.

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20

Mukut, A. N. M. Mominul Islam, Hiroshi Mizunuma, and Obara Hiromichi. "Flow Separation Control Using Plasma Vortex Generator." Procedia Engineering 90 (2014): 232–37. http://dx.doi.org/10.1016/j.proeng.2014.11.842.

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21

Weier, Tom, Gunther Gerbeth, Gerd Mutschke, Olgerts Lielausis, and Gerd Lammers. "Control of Flow Separation Using Electromagnetic Forces." Flow, Turbulence and Combustion (formerly Applied Scientific Research) 71, no. 1-4 (2003): 5–17. http://dx.doi.org/10.1023/b:appl.0000014922.98309.21.

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22

Messanelli, Federico, Edoardo Frigerio, Elia Tescaroli, and Marco Belan. "Flow separation control by pulsed corona actuators." Experimental Thermal and Fluid Science 105 (July 2019): 123–35. http://dx.doi.org/10.1016/j.expthermflusci.2019.03.013.

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23

Hu, Jiaguo, Rugen Wang, Peigen Wu, and Chen He. "Separation Control by Slot Jet in a Critically Loaded Compressor Cascade." International Journal of Turbo & Jet-Engines 35, no. 3 (2018): 229–39. http://dx.doi.org/10.1515/tjj-2016-0044.

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Abstract Separation in compressor cascade triggers flow loss and instability. This paper presents a passive flow control method by introducing a slot into the blade. The slot induces self-adapted jet, while the jet flow is used to suppress cascade’s separation. To study the flow control effect, experiments were conducted and flow field details were given by validated numerical simulations. The results show that a well-designed slot carries adequate jet airflow from pressure side (PS) to suction side (SS) due to the great pressure fall between the two sides. The jet airflow delays suction side

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24

Ayed, Samah Ben, Saad A. Ragab, and Muhammad R. Hajj. "Flow Control of Extreme Pressure Loads Associated with Flow Separation." Journal of Engineering Mechanics 142, no. 2 (2016): 04015068. http://dx.doi.org/10.1061/(asce)em.1943-7889.0000973.

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25

Balasubramanian, R., K. Anandhanarayanan, R. Krishnamurthy, and Debasis Chakraborty. "Mitigation of shock-induced flow separation using magnetohydrodynamic flow control." Sādhanā 42, no. 3 (2017): 379–90. http://dx.doi.org/10.1007/s12046-017-0610-3.

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26

Arai, Fumihito, Akihiko Ichikawa, Toshio Fukuda, Koji Horio, Kouichi Itoigawa, and Keisuke Morishima. "Separation of Target Microbe by Laser Manipulation and Flow Control." Journal of Robotics and Mechatronics 14, no. 2 (2002): 133–39. http://dx.doi.org/10.20965/jrm.2002.p0133.

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We developed random separation of single microorganisms, such as living cells and microbes, in a microfluid device under microscopy using laser manipulation and microchannel flow. The main flow in the microchannel splits at the exit of the sample chamber. One flow goes to the extraction port with high speed to extract the target. Another flow goes to the drain port. The target was transported by laser manipulation from the sample chamber to put on the main flow. Since the force balance of the laser-trapped object is important for stable manipulation of the target, we propose separation point c

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27

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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28

Field, Richard, David Averill, Thomas P. O'Connor, and Paula Steel. "Vortex Separation Technology." Water Quality Research Journal 32, no. 1 (1997): 185–214. http://dx.doi.org/10.2166/wqrj.1997.013.

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Abstract Several types of vortex separators have been developed during the last 30 years. Their major function has been to provide both flow regulation and settleable solids concentration for the control of combined sewer overflows (CSOs). A variety of opinions have developed regarding the application of these technologies, ranging from overwhelming support to reservations of their effectiveness. The performance of vortex devices depends on the settling velocity distribution of the particles in the wastewater. When correctly installed with other controls in combined sewer or separate stormwate

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29

Corke, Thomas C., Patrick O. Bowles, Chuan He, and Eric H. Matlis. "Sensing and control of flow separation using plasma actuators." Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences 369, no. 1940 (2011): 1459–75. http://dx.doi.org/10.1098/rsta.2010.0356.

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Single dielectric barrier discharge plasma actuators have been used to control flow separation in a large number of applications. An often used configuration involves spanwise-oriented asymmetric electrodes that are arranged to induce a tangential wall jet in the mean flow direction. For the best effect, the plasma actuator is placed just upstream of where the flow separation will occur. This approach is generally more effective when the plasma actuator is periodically pulsed at a frequency that scales with the streamwise length of the separation zone and the free-stream velocity. The optimum

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30

Mane, Shreya. "Nozzle Flow Separation Phenomena and Control for different conditions." 3 1, no. 3 (2022): 10–15. http://dx.doi.org/10.46632/jame/1/3/2.

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A detailed study of separated nozzle flows has been conducted. For a subscale, non-axisymmetric, two-dimensional, convergent divergent nozzle, schlieren flow visualization was acquired along with measurements of force, moment, and pressure as part of an extensive static performance evaluation. Additionally, two-dimensional numerical simulations were performed using the computational fluid dynamics package PAB3D together with algebraic Reynold’s stress modelling and two-equation turbulence closure. This study's experimental findings show that shock-induced boundary layer separation, which was c

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31

Ma, Dongli, Guanxiong Li, Muqing Yang, and Shaoqi Wang. "Research of the suction flow control on wings at low Reynolds numbers." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 8 (2017): 1515–28. http://dx.doi.org/10.1177/0954410017694057.

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Laminar separation and transition have significant effects on aerodynamic characteristics of the wing under the condition of low Reynolds numbers. Using the flow control methods to delay and eliminate laminar separation has great significance. This study uses the method combined with water tunnel test and numerical calculation to research the effects of suction flow control on the flow state and aerodynamic force of the wing at low Reynolds numbers. The effects of suction flow rate and suction location on laminar separation, transition and aerodynamic performance of the wing are further resear

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32

Ikenson, Ben. "Pulsative flow improves control of phototactic microswimmers." Scilight 2022, no. 40 (2022): 401103. http://dx.doi.org/10.1063/10.0014488.

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33

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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34

Pan, Jiaxin, Wanbo Wang, Xunnian Wang, Chaoqun Li, Xinhai Zhao, and Kun Tang. "Experimental Investigation on Flow Control over a Circular Cylinder Using Antiphase Pulsed Jets." Actuators 12, no. 12 (2023): 432. http://dx.doi.org/10.3390/act12120432.

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To investigate the flow control characteristics of antiphase pulsed jet technology and explore a more efficient method to control unsteady flow with minimal impact on flow turbulence, wind tunnel experiments were conducted. The aim was to address the issue of flow separation control on the surface of a cylindrical model. The model had a diameter of 100 mm, and an experimental setup utilizing an antiphase pulsed jet excitation was developed. The optimisation of unsteady jet control involved adjusting parameters such as jet momentum coefficient, slot position, and excitation frequency. The flow

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35

Koklu, Mehti, and Lewis R. Owens. "Comparison of Sweeping Jet Actuators with Different Flow-Control Techniques for Flow-Separation Control." AIAA Journal 55, no. 3 (2017): 848–60. http://dx.doi.org/10.2514/1.j055286.

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36

Yi, Weilin, and Lucheng Ji. "Control and Entropy Analysis of Corner Flow Separation in a Compressor Cascade Using Streamwise Grooves." Entropy 21, no. 10 (2019): 928. http://dx.doi.org/10.3390/e21100928.

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Flow separation, which often occurs at the junction of blades and endwalls and seriously limits the aerodynamic performance of turbomachinery, is caused mainly by the boundary layer mixing on the blades and endwall surfaces and the transverse secondary flow. Focusing on a linear diffusion cascade with 42° turning angle, the transverse secondary flow is found to be the dominant factor for flow separation, based on detailed analysis. Therefore, controlling the secondary flow to reduce the flow separation is very important. Based on the investigations, the flow separation can be controlled by cut

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37

Zhu, Shiquan, Zhengui Huang, Yongjie Gou, Qizhong Tang, and Zhihua Chen. "Numerical Investigations on Wedge Control of Separation of a Missile from an Aircraft." Defence Science Journal 68, no. 6 (2018): 583. http://dx.doi.org/10.14429/dsj.68.12552.

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To make the missile safely separate from the internal weapons bay, a wedge flow control device is mounted on the front of the bay to control the variation of flow during the separation. The numerical simulations of missile separation without and with wedge flow control device under different sizes are carried out. The flow fields of different separation processes are obtained and discussed; the aerodynamic parameters and trajectory parameters of missile of different cases are illustrated and compared. Results show that, the wedge flow control device can accelerate the missile separation and ha

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38

Johnston, James P., and Michihiro Nishi. "Vortex generator jets - Means for flow separation control." AIAA Journal 28, no. 6 (1990): 989–94. http://dx.doi.org/10.2514/3.25155.

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39

Ciobaca, V., J. Dandois, and H. Bieler. "A CFD Benchmark for Flow Separation Control Application." International Journal of Flow Control 6, no. 3 (2014): 67–82. http://dx.doi.org/10.1260/1756-8250.6.3.67.

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40

Tesař, V., S. Zhong, and F. Rasheed. "New Fluidic-Oscillator Concept for Flow-Separation Control." AIAA Journal 51, no. 2 (2013): 397–405. http://dx.doi.org/10.2514/1.j051791.

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41

Pinier, Jeremy T., Julie M. Ausseur, Mark N. Glauser, and Hiroshi Higuchi. "Proportional Closed-Loop Feedback Control of Flow Separation." AIAA Journal 45, no. 1 (2007): 181–90. http://dx.doi.org/10.2514/1.23465.

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42

Greenblatt, David, and Israel J. Wygnanski. "The control of flow separation by periodic excitation." Progress in Aerospace Sciences 36, no. 7 (2000): 487–545. http://dx.doi.org/10.1016/s0376-0421(00)00008-7.

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43

ABE, Hiroyuki, Takehiro NOMURA, Yoshihiro KIKUSHIMA, and Hiro YOSHIDA. "Smart Control of Flow Separation around an Airfoil." Journal of Power and Energy Systems 2, no. 3 (2008): 1036–47. http://dx.doi.org/10.1299/jpes.2.1036.

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44

Rosenblum, J. P., P. Vrchota, A. Prachar, et al. "Active flow separation control at the outer wing." CEAS Aeronautical Journal 11, no. 4 (2019): 823–36. http://dx.doi.org/10.1007/s13272-019-00402-4.

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45

Sankar, Hari, and A. M. Pradeep. "Improvement of effectiveness of EMHD flow separation control." Journal of the Brazilian Society of Mechanical Sciences and Engineering 39, no. 10 (2017): 3947–63. http://dx.doi.org/10.1007/s40430-017-0880-z.

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46

Warsop, Clyde, Martyn Hucker, Andrew J. Press, and Paul Dawson. "Pulsed Air-jet Actuators for Flow Separation Control." Flow, Turbulence and Combustion 78, no. 3-4 (2007): 255–81. http://dx.doi.org/10.1007/s10494-006-9060-4.

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47

Greenblatt, David, Torsten Schneider, and Chan Yong Schüle. "Mechanism of flow separation control using plasma actuation." Physics of Fluids 24, no. 7 (2012): 077102. http://dx.doi.org/10.1063/1.4733399.

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48

Choi, Byunghun, Youkyung Hong, Byunghyun Lee, Minhee Kim, H. Jin Kim, and Chongam Kim. "Adaptive Flow Separation Control Over an Asymmetric Airfoil." International Journal of Aeronautical and Space Sciences 19, no. 2 (2018): 305–15. http://dx.doi.org/10.1007/s42405-018-0029-z.

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49

Li, Bo, Xuanshi Meng, Shiqing Yin, Weiwei Hui, and Huaxing Li. "Flow Separation Control over an Airfoil Using Plasma Co-Flow Jet." AIAA Journal 60, no. 4 (2022): 2195–206. http://dx.doi.org/10.2514/1.j060911.

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50

Liu, Wenbo, Qikai Qin, Yongwei Liu, Keming Wu, Qi Zhou, and Dejiang Shang. "Effect of wall heating on flow-induced structure vibration noise of an underwater wing structure." Journal of Physics: Conference Series 3007, no. 1 (2025): 012059. https://doi.org/10.1088/1742-6596/3007/1/012059.

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Abstract This paper investigates the control effect of wall heating on turbulent pressure fluctuations and flow-induced structure vibration noise in a wing structures through numerical calculations. The control mechanism of wall heating is examined through turbulent kinetic energy distribution, the flow separation location, and the three-dimensional vortex structure. The flow and sound fields are solved employing the large-eddy simulation (LES) method and a hybrid numerical method, respectively. Numerical calculation results show that wall heating delays the flow separation and shortens the de

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