Numerical simulation of flow-induced vibration of two cylinders elastically mounted in tandem by immersed moving boundary method

•Coupling Immersed Moving Boundary Method with high-precision fluid solver.•Proposing a modified Poisson equation, for pressure, to simulate moving bodies represented by an immersed boundary method.•Consistent representation of resonance and wake-flutter phenomena of elastically-mounted cylinders in...

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Veröffentlicht in:Applied Mathematical Modelling 2020-01, Vol.77, p.1331-1347
Hauptverfasser: Narváez, G.F., Schettini, E.B., Silvestrini, J.H.
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Schettini, E.B.
Silvestrini, J.H.
description •Coupling Immersed Moving Boundary Method with high-precision fluid solver.•Proposing a modified Poisson equation, for pressure, to simulate moving bodies represented by an immersed boundary method.•Consistent representation of resonance and wake-flutter phenomena of elastically-mounted cylinders in tandem arrangement.•Confinement effect on the rear cylinder, in which the upstream wake acts as a damper on the rear cylinder.•Streamwise oscillations are not negligible in comparison with the cross-stream oscillations. A numerical study is performed on flow-induced vibrations of two cylinders of diameter D, in tandem configuration relative to the free-stream uniform flow U at low Reynolds numbers Re=UD/ν. In order to solve numerically the incompressible momentum and continuity equations, the in-house code Incompact3D is used. Compact sixth-order finite differences for spatial differentiation and second-order Adams–Bashforth scheme for time advancement are employed. The cylinders movement is modeled as a mass-damper-spring system which is solved by a fourth-order Runge–Kutta scheme. To represent the multiple moving cylinders in an immersed boundary method framework, a modification in the Poisson equation is proposed. The modified algorithm was evaluated and applied for scenarios with zero, one and two translational degrees of freedom to oscillate. The validation is carried out against several numerical and experimental previous works. The results are analyzed in terms of the forces on cylinders, Strouhal number of the wake, streamwise velocity profiles and cylinders oscillation amplitudes and frequencies. The algorithm could satisfactorily represent the resonance and wake-flutter phenomena. In the most cases, the rear cylinder has greater oscillations than the front cylinder. However, a state was identified where the cross-stream oscillation amplitudes of the front cylinder are lower than those of the rear cylinder. In this state, the lift force acts as negative spring on the front cylinder (amplifying its oscillations) and as a damper on the rear cylinder (controlling its oscillations). The scenarios with two degrees of freedom (2dof) have higher oscillation amplitudes than the equivalent scenarios with one degree of freedom. Moreover, the streamwise oscillation amplitudes are not negligible in relation to the cross-stream oscillation amplitudes. On the other hand, for 2dof, when the Reynolds number increases the clashing risk also increases, since the cylinde
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A numerical study is performed on flow-induced vibrations of two cylinders of diameter D, in tandem configuration relative to the free-stream uniform flow U at low Reynolds numbers Re=UD/ν. In order to solve numerically the incompressible momentum and continuity equations, the in-house code Incompact3D is used. Compact sixth-order finite differences for spatial differentiation and second-order Adams–Bashforth scheme for time advancement are employed. The cylinders movement is modeled as a mass-damper-spring system which is solved by a fourth-order Runge–Kutta scheme. To represent the multiple moving cylinders in an immersed boundary method framework, a modification in the Poisson equation is proposed. The modified algorithm was evaluated and applied for scenarios with zero, one and two translational degrees of freedom to oscillate. The validation is carried out against several numerical and experimental previous works. The results are analyzed in terms of the forces on cylinders, Strouhal number of the wake, streamwise velocity profiles and cylinders oscillation amplitudes and frequencies. The algorithm could satisfactorily represent the resonance and wake-flutter phenomena. In the most cases, the rear cylinder has greater oscillations than the front cylinder. However, a state was identified where the cross-stream oscillation amplitudes of the front cylinder are lower than those of the rear cylinder. In this state, the lift force acts as negative spring on the front cylinder (amplifying its oscillations) and as a damper on the rear cylinder (controlling its oscillations). The scenarios with two degrees of freedom (2dof) have higher oscillation amplitudes than the equivalent scenarios with one degree of freedom. Moreover, the streamwise oscillation amplitudes are not negligible in relation to the cross-stream oscillation amplitudes. 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A numerical study is performed on flow-induced vibrations of two cylinders of diameter D, in tandem configuration relative to the free-stream uniform flow U at low Reynolds numbers Re=UD/ν. In order to solve numerically the incompressible momentum and continuity equations, the in-house code Incompact3D is used. Compact sixth-order finite differences for spatial differentiation and second-order Adams–Bashforth scheme for time advancement are employed. The cylinders movement is modeled as a mass-damper-spring system which is solved by a fourth-order Runge–Kutta scheme. To represent the multiple moving cylinders in an immersed boundary method framework, a modification in the Poisson equation is proposed. The modified algorithm was evaluated and applied for scenarios with zero, one and two translational degrees of freedom to oscillate. The validation is carried out against several numerical and experimental previous works. The results are analyzed in terms of the forces on cylinders, Strouhal number of the wake, streamwise velocity profiles and cylinders oscillation amplitudes and frequencies. The algorithm could satisfactorily represent the resonance and wake-flutter phenomena. In the most cases, the rear cylinder has greater oscillations than the front cylinder. However, a state was identified where the cross-stream oscillation amplitudes of the front cylinder are lower than those of the rear cylinder. In this state, the lift force acts as negative spring on the front cylinder (amplifying its oscillations) and as a damper on the rear cylinder (controlling its oscillations). The scenarios with two degrees of freedom (2dof) have higher oscillation amplitudes than the equivalent scenarios with one degree of freedom. Moreover, the streamwise oscillation amplitudes are not negligible in relation to the cross-stream oscillation amplitudes. On the other hand, for 2dof, when the Reynolds number increases the clashing risk also increases, since the cylinders proximity is narrowed.</description><subject>Algorithms</subject><subject>Amplitudes</subject><subject>Computational fluid dynamics</subject><subject>Computer simulation</subject><subject>Continuity equation</subject><subject>Cylinders</subject><subject>Degrees of freedom</subject><subject>Flow generated vibrations</subject><subject>Flow-induced vibration</subject><subject>Fluid flow</subject><subject>Flutter</subject><subject>Immersed boundary method</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Numerical simulation</subject><subject>Oscillations</subject><subject>Poisson equation</subject><subject>Reynolds number</subject><subject>Runge-Kutta method</subject><subject>Strouhal number</subject><subject>Tandem configuration</subject><subject>Tandem cylinders</subject><subject>Uniform flow</subject><subject>Velocity distribution</subject><issn>0307-904X</issn><issn>1088-8691</issn><issn>0307-904X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNp9UEtLxDAQDqLguvoDvAU8t07S9IUnWXzBohcFbyFNUk1pmzVJV_bmTzdlRTwJAzPJ95jhQ-icQEqAFJddKjZDSoHUKcSC8gAtIIMyqYG9Hv6Zj9GJ9x0A5PG1QF-P06CdkaLH3gxTL4KxI7Ytbnv7mZhRTVIrvDWN-0XCp8Vy10dMO491L3yY9f0OD3YaQ6SbEQcR4QE3O2yGuMDH38FuzfiGm0hSwkW2Du9WnaKjVvRen_30JXq5vXle3Sfrp7uH1fU6kVlRhaQWNatKVsqa5qVqhaRVJalSjaRZlgFUeUNpVlNBWNs0TLWkYKxuKkbLjLGizJboYu-7cfZj0j7wzk5ujCv57DC713lkkT1LOuu90y3fODPEazkBPgfNOx6D5nPQHGLB7Hy11-h4_tZox700eoy5Gadl4Mqaf9TfEQ-IWw</recordid><startdate>202001</startdate><enddate>202001</enddate><creator>Narváez, G.F.</creator><creator>Schettini, E.B.</creator><creator>Silvestrini, J.H.</creator><general>Elsevier Inc</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>8FD</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0001-9387-4564</orcidid></search><sort><creationdate>202001</creationdate><title>Numerical simulation of flow-induced vibration of two cylinders elastically mounted in tandem by immersed moving boundary method</title><author>Narváez, G.F. ; Schettini, E.B. ; Silvestrini, J.H.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c368t-9a948747c9257dfac288c2ddbc23330085b22392a14fbb4df16449b8427344673</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Algorithms</topic><topic>Amplitudes</topic><topic>Computational fluid dynamics</topic><topic>Computer simulation</topic><topic>Continuity equation</topic><topic>Cylinders</topic><topic>Degrees of freedom</topic><topic>Flow generated vibrations</topic><topic>Flow-induced vibration</topic><topic>Fluid flow</topic><topic>Flutter</topic><topic>Immersed boundary method</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Numerical simulation</topic><topic>Oscillations</topic><topic>Poisson equation</topic><topic>Reynolds number</topic><topic>Runge-Kutta method</topic><topic>Strouhal number</topic><topic>Tandem configuration</topic><topic>Tandem cylinders</topic><topic>Uniform flow</topic><topic>Velocity distribution</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Narváez, G.F.</creatorcontrib><creatorcontrib>Schettini, E.B.</creatorcontrib><creatorcontrib>Silvestrini, J.H.</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts – Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Applied Mathematical Modelling</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Narváez, G.F.</au><au>Schettini, E.B.</au><au>Silvestrini, J.H.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical simulation of flow-induced vibration of two cylinders elastically mounted in tandem by immersed moving boundary method</atitle><jtitle>Applied Mathematical Modelling</jtitle><date>2020-01</date><risdate>2020</risdate><volume>77</volume><spage>1331</spage><epage>1347</epage><pages>1331-1347</pages><issn>0307-904X</issn><issn>1088-8691</issn><eissn>0307-904X</eissn><abstract>•Coupling Immersed Moving Boundary Method with high-precision fluid solver.•Proposing a modified Poisson equation, for pressure, to simulate moving bodies represented by an immersed boundary method.•Consistent representation of resonance and wake-flutter phenomena of elastically-mounted cylinders in tandem arrangement.•Confinement effect on the rear cylinder, in which the upstream wake acts as a damper on the rear cylinder.•Streamwise oscillations are not negligible in comparison with the cross-stream oscillations. A numerical study is performed on flow-induced vibrations of two cylinders of diameter D, in tandem configuration relative to the free-stream uniform flow U at low Reynolds numbers Re=UD/ν. In order to solve numerically the incompressible momentum and continuity equations, the in-house code Incompact3D is used. Compact sixth-order finite differences for spatial differentiation and second-order Adams–Bashforth scheme for time advancement are employed. The cylinders movement is modeled as a mass-damper-spring system which is solved by a fourth-order Runge–Kutta scheme. To represent the multiple moving cylinders in an immersed boundary method framework, a modification in the Poisson equation is proposed. The modified algorithm was evaluated and applied for scenarios with zero, one and two translational degrees of freedom to oscillate. The validation is carried out against several numerical and experimental previous works. The results are analyzed in terms of the forces on cylinders, Strouhal number of the wake, streamwise velocity profiles and cylinders oscillation amplitudes and frequencies. The algorithm could satisfactorily represent the resonance and wake-flutter phenomena. In the most cases, the rear cylinder has greater oscillations than the front cylinder. However, a state was identified where the cross-stream oscillation amplitudes of the front cylinder are lower than those of the rear cylinder. In this state, the lift force acts as negative spring on the front cylinder (amplifying its oscillations) and as a damper on the rear cylinder (controlling its oscillations). The scenarios with two degrees of freedom (2dof) have higher oscillation amplitudes than the equivalent scenarios with one degree of freedom. Moreover, the streamwise oscillation amplitudes are not negligible in relation to the cross-stream oscillation amplitudes. On the other hand, for 2dof, when the Reynolds number increases the clashing risk also increases, since the cylinders proximity is narrowed.</abstract><cop>New York</cop><pub>Elsevier Inc</pub><doi>10.1016/j.apm.2019.09.007</doi><tpages>17</tpages><orcidid>https://orcid.org/0000-0001-9387-4564</orcidid><oa>free_for_read</oa></addata></record>
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subjects Algorithms
Amplitudes
Computational fluid dynamics
Computer simulation
Continuity equation
Cylinders
Degrees of freedom
Flow generated vibrations
Flow-induced vibration
Fluid flow
Flutter
Immersed boundary method
Mathematical analysis
Mathematical models
Numerical simulation
Oscillations
Poisson equation
Reynolds number
Runge-Kutta method
Strouhal number
Tandem configuration
Tandem cylinders
Uniform flow
Velocity distribution
title Numerical simulation of flow-induced vibration of two cylinders elastically mounted in tandem by immersed moving boundary method
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