Unsteadiness control of laminar junction flows on pressure fluctuations
Smoke-wire flow visualization is conducted carefully in a laminar junction to explore the physical behavior of laminar junction flows. The two-dimensional (2D) velocity fields in the 30° plane of a laminar junction flow are acquired by a time-resolved particle image velocimetry (PIV) system at a fra...
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| Published in | Applied mathematics and mechanics Vol. 40; no. 3; pp. 373 - 380 |
|---|---|
| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
| Published |
Shanghai
Shanghai University
01.03.2019
Springer Nature B.V National Key Laboratory on Ship Vibration & Noise, Wuxi 214082,Jiangsu Province, China%Space Research Institute of Russian Academy of Sciences, Moscow 117997, Russia%China Ship Scientific Research Center, Wuxi 214082, Jiangsu Province, China China Ship Scientific Research Center, Wuxi 214082, Jiangsu Province, China |
| Edition | English ed. |
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| Online Access | Get full text |
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| Abstract | Smoke-wire flow visualization is conducted carefully in a laminar junction to explore the physical behavior of laminar junction flows. The two-dimensional (2D) velocity fields in the 30° plane of a laminar junction flow are acquired by a time-resolved particle image velocimetry (PIV) system at a frame rate of 1 kHz, based on which the unsteady fluctuating pressure fields can be calculated by the multi-path integration method proposed in the literature (GAND, F., DECK, S., BRUNET,V., and SAGAUT, P. Flow dynamics past a simplified wing body junction.
Physics of Fluids
,
22
(11), 115111 (2010)). A novel control strategy is utilized to attenuate the unsteadiness of the horseshoe vortices of the laminar junction flow, and the consequent effect on pressure fields is analyzed. |
|---|---|
| AbstractList | Smoke-wire flow visualization is conducted carefully in a laminar junction to explore the physical behavior of laminar junction flows. The two-dimensional (2D) velocity fields in the 30° plane of a laminar junction flow are acquired by a time-resolved particle image velocimetry (PIV) system at a frame rate of 1 kHz, based on which the unsteady fluctuating pressure fields can be calculated by the multi-path integration method proposed in the literature (GAND, F., DECK, S., BRUNET,V., and SAGAUT, P. Flow dynamics past a simplified wing body junction.
Physics of Fluids
,
22
(11), 115111 (2010)). A novel control strategy is utilized to attenuate the unsteadiness of the horseshoe vortices of the laminar junction flow, and the consequent effect on pressure fields is analyzed. O357.4; Smoke-wire flow visualization is conducted carefully in a laminar junction to explore the physical behavior of laminar junction flows.The two-dimensional (2D)velocity fields in the 30° plane of a laminar junction flow are acquired by a time-resolved particle image velocimetry (PIV) system at a frame rate of 1 kHz,based on which the unsteady fluctuating pressure fields can be calculated by the multi-path integration method proposed in the literature (GAND,F.,DECK,S.,BRUNET,V.,and SAGAUT,P.Flow dynamics past a simplified wing body junction.Physics of Fluids,22(11),115111 (2010)).A novel control strategy is utilized to attenuate the unsteadiness of the horseshoe vortices of the laminar junction flow,and the consequent effect on pressure fields is analyzed. Smoke-wire flow visualization is conducted carefully in a laminar junction to explore the physical behavior of laminar junction flows. The two-dimensional (2D) velocity fields in the 30° plane of a laminar junction flow are acquired by a time-resolved particle image velocimetry (PIV) system at a frame rate of 1 kHz, based on which the unsteady fluctuating pressure fields can be calculated by the multi-path integration method proposed in the literature (GAND, F., DECK, S., BRUNET,V., and SAGAUT, P. Flow dynamics past a simplified wing body junction. Physics of Fluids, 22(11), 115111 (2010)). A novel control strategy is utilized to attenuate the unsteadiness of the horseshoe vortices of the laminar junction flow, and the consequent effect on pressure fields is analyzed. |
| Author | Zhai, Shucheng Kudashev, E. Hong, Fangwen Liu, Jianhua Yan, Kai |
| AuthorAffiliation | China Ship Scientific Research Center, Wuxi 214082, Jiangsu Province, China;National Key Laboratory on Ship Vibration & Noise, Wuxi 214082,Jiangsu Province, China%Space Research Institute of Russian Academy of Sciences, Moscow 117997, Russia%China Ship Scientific Research Center, Wuxi 214082, Jiangsu Province, China |
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| Author_xml | – sequence: 1 givenname: Jianhua surname: Liu fullname: Liu, Jianhua email: jhliu@cssrc.com.cn organization: China Ship Scientific Research Center, National Key Laboratory on Ship Vibration & Noise – sequence: 2 givenname: Shucheng surname: Zhai fullname: Zhai, Shucheng organization: China Ship Scientific Research Center, National Key Laboratory on Ship Vibration & Noise – sequence: 3 givenname: E. surname: Kudashev fullname: Kudashev, E. organization: Space Research Institute of Russian Academy of Sciences – sequence: 4 givenname: Fangwen surname: Hong fullname: Hong, Fangwen organization: China Ship Scientific Research Center, National Key Laboratory on Ship Vibration & Noise – sequence: 5 givenname: Kai surname: Yan fullname: Yan, Kai organization: China Ship Scientific Research Center |
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| References | Devenpor, Simpson (CR8) 1990; 210 Piquet (CR7) 1999 Paik, Escauriaza, Sotiropoulos (CR3) 2007; 19 Paik-Aider, Beaudoin, Wesfreid (CR4) 2010; 48 Kirkil, Constantinescu, Ettema (CR6) 2008; 134 Wang, Bi, Wei (CR10) 2009; 46 Dabiri, Bose, Gemmell, Colin, Costello (CR11) 2014; 217 Gand, Deck, Brunet, Sagaut (CR2) 2010; 22 Doolan, Coombs, Moreau, Zander (CR5) 2012 Simpson (CR1) 2001; 33 Jukes, Choi (CR9) 2013; 733 T. W. J. Devenpor (2447_CR8) 1990; 210 T. N. Jukes (2447_CR9) 2013; 733 G. Kirkil (2447_CR6) 2008; 134 J. Piquet (2447_CR7) 1999 J. L. Paik-Aider (2447_CR4) 2010; 48 J. O. Dabiri (2447_CR11) 2014; 217 R. L. Simpson (2447_CR1) 2001; 33 C. J. Doolan (2447_CR5) 2012 J. Paik (2447_CR3) 2007; 19 F. Gand (2447_CR2) 2010; 22 J. M. Wang (2447_CR10) 2009; 46 |
| References_xml | – volume: 48 start-page: 771 year: 2010 end-page: 789 ident: CR4 article-title: Drag and lift reduction of a 3D blunt-body using active vortex generators publication-title: Experiments in Fluids doi: 10.1007/s00348-009-0770-y contributor: fullname: Wesfreid – volume: 210 start-page: 23 year: 1990 end-page: 55 ident: CR8 article-title: Time-dependent and time-averaged turbulence structure near the nose of a wing-body junction publication-title: Journal of Fluid Mechanics doi: 10.1017/S0022112090001215 contributor: fullname: Simpson – volume: 19 start-page: 045107 year: 2007 ident: CR3 article-title: On the bimodal dynamics of the turbu-lent horseshoe vortex system in a wing-body junction publication-title: Physics of Fluids doi: 10.1063/1.2716813 contributor: fullname: Sotiropoulos – volume: 217 start-page: 331 year: 2014 end-page: 336 ident: CR11 article-title: An algorithm to estimate unsteady and quasi-steady pressure fields from velocity field measurements publication-title: Journal of Experimental Biology doi: 10.1242/jeb.092767 contributor: fullname: Costello – volume: 46 start-page: 1093 year: 2009 end-page: 1104 ident: CR10 article-title: Effects of an upstream inclined rod on the circular cylinder at plate junction flow publication-title: Experiments in Fluids doi: 10.1007/s00348-009-0619-4 contributor: fullname: Wei – volume: 733 start-page: 370 year: 2013 end-page: 393 ident: CR9 article-title: On the formation of streamwise vortices by plasma vortex gener-ators publication-title: Journal of Fluid Mechanics doi: 10.1017/jfm.2013.418 contributor: fullname: Choi – year: 2012 ident: CR5 publication-title: Prediction of noise from a wing-in-junction flow using computational fluid dynamics contributor: fullname: Zander – volume: 22 start-page: 115111 year: 2010 ident: CR2 article-title: Flow dynamics past a simplified wing body junction publication-title: Physics of Fluids doi: 10.1063/1.3500697 contributor: fullname: Sagaut – year: 1999 ident: CR7 publication-title: Complex effects in turbulent flows doi: 10.1007/978-3-662-03559-7 contributor: fullname: Piquet – volume: 33 start-page: 415 year: 2001 end-page: 443 ident: CR1 article-title: Junction flows publication-title: Annual Review of Fluid Mechanics doi: 10.1146/annurev.fluid.33.1.415 contributor: fullname: Simpson – volume: 134 start-page: 572 year: 2008 end-page: 587 ident: CR6 article-title: Coherent structures in the flow field around a circular cylinder with scour hole publication-title: Journal of Hydraulic Engineering doi: 10.1061/(ASCE)0733-9429(2008)134:5(572) contributor: fullname: Ettema – volume: 46 start-page: 1093 year: 2009 ident: 2447_CR10 publication-title: Experiments in Fluids doi: 10.1007/s00348-009-0619-4 contributor: fullname: J. M. Wang – volume: 134 start-page: 572 year: 2008 ident: 2447_CR6 publication-title: Journal of Hydraulic Engineering doi: 10.1061/(ASCE)0733-9429(2008)134:5(572) contributor: fullname: G. Kirkil – volume: 19 start-page: 045107 year: 2007 ident: 2447_CR3 publication-title: Physics of Fluids doi: 10.1063/1.2716813 contributor: fullname: J. Paik – volume: 33 start-page: 415 year: 2001 ident: 2447_CR1 publication-title: Annual Review of Fluid Mechanics doi: 10.1146/annurev.fluid.33.1.415 contributor: fullname: R. L. Simpson – volume: 733 start-page: 370 year: 2013 ident: 2447_CR9 publication-title: Journal of Fluid Mechanics doi: 10.1017/jfm.2013.418 contributor: fullname: T. N. Jukes – volume: 217 start-page: 331 year: 2014 ident: 2447_CR11 publication-title: Journal of Experimental Biology doi: 10.1242/jeb.092767 contributor: fullname: J. O. Dabiri – volume-title: Prediction of noise from a wing-in-junction flow using computational fluid dynamics year: 2012 ident: 2447_CR5 contributor: fullname: C. J. Doolan – volume-title: Complex effects in turbulent flows year: 1999 ident: 2447_CR7 doi: 10.1007/978-3-662-03559-7 contributor: fullname: J. Piquet – volume: 48 start-page: 771 year: 2010 ident: 2447_CR4 publication-title: Experiments in Fluids doi: 10.1007/s00348-009-0770-y contributor: fullname: J. L. Paik-Aider – volume: 210 start-page: 23 year: 1990 ident: 2447_CR8 publication-title: Journal of Fluid Mechanics doi: 10.1017/S0022112090001215 contributor: fullname: T. W. J. Devenpor – volume: 22 start-page: 115111 year: 2010 ident: 2447_CR2 publication-title: Physics of Fluids doi: 10.1063/1.3500697 contributor: fullname: F. Gand |
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| Snippet | Smoke-wire flow visualization is conducted carefully in a laminar junction to explore the physical behavior of laminar junction flows. The two-dimensional (2D)... O357.4; Smoke-wire flow visualization is conducted carefully in a laminar junction to explore the physical behavior of laminar junction flows.The... |
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| SubjectTerms | Applications of Mathematics Classical Mechanics Flow visualization Fluid dynamics Fluid flow Fluid- and Aerodynamics Horseshoe vortices Image acquisition Laminar flow Mathematical Modeling and Industrial Mathematics Mathematics Mathematics and Statistics Partial Differential Equations Particle image velocimetry Pressure effects Smoke Two dimensional flow Variation Velocity distribution Velocity measurement |
| Title | Unsteadiness control of laminar junction flows on pressure fluctuations |
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