SIMULATION OF FLUID-SOLID INTERACTION ON WATER DITCHING OF AN AIRPLANE BY ALE METHOD
Ditching is considered as one of the important aspects of safety performances of airplanes. It is related primarily with the fluid-solid interaction, whose studies mainly depend on experiments at the present time. Numerical and analytical methods for fluid-solid interaction by using 3-D full scale a...
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Published in | Journal of hydrodynamics. Series B Vol. 23; no. 5; pp. 637 - 642 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Singapore
Elsevier Ltd
01.10.2011
Springer Singapore Department of Mechanics and Engineering Science, Fudan University, Shanghai 200433, China%School of Mathematical Sciences, Fudan University, Shanghai 200433, China |
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Abstract | Ditching is considered as one of the important aspects of safety performances of airplanes. It is related primarily with the fluid-solid interaction, whose studies mainly depend on experiments at the present time. Numerical and analytical methods for fluid-solid interaction by using 3-D full scale airplane's model will reduce the dependence on the expensive model tests. Numerical studies can be used to estimate the safety of ditching and provide a reference for the crashworthiness design. This article proposes a 3-D dynamical structural model after the real shape of an airplane and an Arbitrary Lagrange-Euler (ALE) fluid-field model, to simulate the fluid-solid interactions caused by low speed ditching. The simulation is based on interaction computational methods, within LS-DYNA nonlinear finite-element code. The results of pressure distributions and accelerating time histories of the airplane's subfloor are discussed in the context of the safety of ditching, and the simulation results and the analytical methods are verified. |
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AbstractList | Ditching is considered as one of the important aspects of safety performances of airplanes. It is related primarily with the fluid-solid interaction, whose studies mainly depend on experiments at the present time. Numerical and analytical methods for fluid-solid interaction by using 3-D full scale airplane's model will reduce the dependence on the expensive model tests. Numerical studies can be used to estimate the safety of ditching and provide a reference for the crashworthiness design. This article proposes a 3-D dynamical structural model after the real shape of an airplane and an Arbitrary Lagrange-Euler (ALE) fluid-field model, to simulate the fluid-solid interactions caused by low speed ditching. The simulation is based on interaction computational methods, within LS-DYNA nonlinear finite-element code. The results of pressure distributions and accelerating time histories of the airplane's subfloor are discussed in the context of the safety of ditching, and the simulation results and the analytical methods are verified. V216.5; Ditching is considered as one of the important aspects of safety performances of airplanes.It is related primarily with the fluid-solid interaction,whose studies mainly depend on experiments at the present time.Numerical and analytical methods for fluid-solid interaction by using 3-D full scale airplane's model will reduce the dependence on the expensive model tests.Numerical studies can be used to estimate the safety of ditching and provide a reference for the crashworthiness design.This article proposes a 3-D dynamical structural model after the real shape of an airplane and an Arbitrary Lagrange-Euler (ALE) fluid-field model,to simulate the fluid-solid interactions caused by low speed ditching.The simulation is based on interaction computational methods,within LS-DYNA nonlinear finite-element code.The results of pressure distributions and accelerating time histories of the airplane's subfloor are discussed in the context of the safety of ditching,and the simulation results and the analytical methods are verified. Ditching is considered as one of the important aspects of safety performances of airplanes. It is related primarily with the fluid-solid interaction, whose studies mainly depend on experiments at the present time. Numerical and analytical methods for fluid-solid interaction by using 3-D full scale airplane's model will reduce the dependence on the expensive model tests. Numerical studies can be used to estimate the safety of ditching and provide a reference for the crashworthiness design. This article proposes a 3-D dynamical structural model after the real shape of an airplane and an Arbitrary Lagrange-Euler (ALE) fluid-field model, to simulate the fluid-solid interactions caused by low speed ditching. The simulation is based on interaction computational methods, within LS-DYNA nonlinear finite-element code. The results of pressure distributions and accelerating time histories of the airplane's subfloor are discussed in the context of the safety of ditching, and the simulation results and the analytical methods are verified. |
Author | HUA Cheng FANG Chao CHENG Jin |
AuthorAffiliation | Department of Mechanics and Engineering Science, Fudan University, Shanghai 200433, China, School of Mathematical Sciences, Fudan University, Shanghai 200433, China |
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Cites_doi | 10.1016/0045-7825(81)90049-9 10.1016/0021-9991(74)90051-5 10.1016/j.ijimpeng.2004.09.002 10.2514/3.26468 10.1016/S1001-6058(08)60209-7 10.1016/S0045-7825(99)00432-6 |
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Keywords | fluid structure interaction finite element method Arbitrary Lagrange-Euler (ALE) ditching fmite element method |
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Notes | 31-1563/T Ditching is considered as one of the important aspects of safety performances of airplanes. It is related primarily with the fluid-solid interaction, whose studies mainly depend on experiments at the present time. Numerical and analytical methods for fluid-solid interaction by using 3-D full scale airplane's model will reduce the dependence on the expensive model tests. Numerical studies can be used to estimate the safety of ditching and provide a reference for the crashworthiness design. This article proposes a 3-D dynamical structural model after the real shape of an airplane and an Arbitrary Lagrange-Euler (ALE) fluid-field model, to simulate the fluid-solid interactions caused by low speed ditching. The simulation is based on interaction computational methods, within LS-DYNA nonlinear finite-element code. The results of pressure distributions and accelerating time histories of the airplane's subfloor are discussed in the context of the safety of ditching, and the simulation results and the analytical methods are verified. ditching, fluid structure interaction, Arbitrary Lagrange-Euler (ALE), finite element method ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
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A contributor: fullname: LIU – volume: 29 start-page: 329 year: 1981 end-page: 349 ident: bib11 article-title: Lagrangian Eulerian finite elements formulation for viscous flows[J] publication-title: Computer Methods in Applied Mechanics and Engineering contributor: fullname: ZIMMERMAN – volume: 14 start-page: 227 year: 1974 end-page: 253 ident: bib4 article-title: An arbitrary Lagrangian-Eulerian method for all flow speeds[J] publication-title: Journal of Computational Physics contributor: fullname: COOK – start-page: 181 year: 2004 end-page: 189 ident: bib10 article-title: ALE and fluid/structure interaction in LS-DYNA[J] publication-title: American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP contributor: fullname: OLOVSSON – volume: 18 start-page: 104 year: 2003 end-page: 109 ident: bib7 article-title: Experimental research on the fluid-structure interaction in water entry of 2D elastic wedge[J] publication-title: Journal of Hydrodynamics, Ser. A contributor: fullname: He – volume: 31 start-page: 509 year: 1994 end-page: 515 ident: bib3 article-title: Dynamics of a space module impacting water[J] publication-title: Spacecraft Rockets contributor: fullname: ANDERSON – volume: 190 start-page: 659 year: 2000 end-page: 675 ident: bib12 article-title: ALE formulation for fluid-structure interaction problems[J] publication-title: Computer Methods in Applied Mechanics and Engineering contributor: fullname: LEWIN – volume: 29 start-page: 329 issue: 3 year: 1981 end-page: 349 ident: CR11 article-title: Lagrangian Eulerian finite elements formulation for viscous flows[J] publication-title: Computer Methods in Applied Mechanics and Engineering doi: 10.1016/0045-7825(81)90049-9 contributor: fullname: Zimmerman – year: 2004 ident: CR5 article-title: The use of LS-DYNA to simulate the water landing characteristics of space vehicles[C] publication-title: 8th International LS-DYNA Users Conference Fluid/Structure contributor: fullname: Taylor – volume: 14 start-page: 227 issue: 3 year: 1974 end-page: 253 ident: CR4 article-title: An arbitrary Lagrangian-Eulerian method for all flow speeds[J] publication-title: Journal of Computational Physics doi: 10.1016/0021-9991(74)90051-5 contributor: fullname: Cook – volume: 32 start-page: 1045 issue: 7 year: 2006 end-page: 1067 ident: CR2 article-title: Review of water entry with applications to aerospace structures[J] publication-title: International Journal of Impact Engineering doi: 10.1016/j.ijimpeng.2004.09.002 contributor: fullname: Moatamedi – volume: 31 start-page: 509 issue: 3 year: 1994 end-page: 515 ident: CR3 article-title: Dynamics of a space module impacting water[J] publication-title: Spacecraft Rockets doi: 10.2514/3.26468 contributor: fullname: Anderson – volume: 21 start-page: 750 issue: 6 year: 2009 end-page: 757 ident: CR8 article-title: Water entry of a wedge based on SPH model with an improved boundary treatment[J] publication-title: Journal of Hydrodynamics doi: 10.1016/S1001-6058(08)60209-7 contributor: fullname: Wang – volume: 28 start-page: 718 issue: 5 year: 2010 end-page: 723 ident: CR9 article-title: Exploring high-speed oblique water entry impact of an underwater vehicle[J] publication-title: Journal of Northwestern Polytechnical University contributor: fullname: Wang – start-page: 19 year: 2007 end-page: 27 ident: CR1 article-title: The ditching study of airworthi ness certification of civil aircraft[J] publication-title: Civil Aircraft Design and Research contributor: fullname: Tian – year: 2005 ident: CR15 article-title: Fluid structure interaction for immersed bodies[C] publication-title: 6th European LS-DYNA Users’Conference contributor: fullname: Chen – year: 2008 ident: CR13 article-title: Comparison of ALE and SPH simulations of vertical drop tests of a composite fuselage section into water[C] publication-title: 10th International LS-DYNA Users Conference contributor: fullname: Yvonne – volume: 18 start-page: 104 issue: 1 year: 2003 end-page: 109 ident: CR7 article-title: Experimental research on the fluid-structure interaction in water entry of 2D elastic wedge[J] publication-title: Journal of Hydrodynamics, Ser. A contributor: fullname: He – start-page: 181 year: 2004 end-page: 189 ident: CR10 article-title: ALE and fluid/structure interaction in LS-DYNA[J] publication-title: American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP contributor: fullname: Olovsson – volume: 18 start-page: 463 issue: 4 year: 2003 end-page: 469 ident: CR14 article-title: ALE finite element method for free surface Navier-Stokes flow using fractional step methods[J] publication-title: Journal of Hydrodynamics, Ser. A contributor: fullname: Liu – volume: 33 start-page: 1117 issue: 9 year: 2007 end-page: 1120 ident: CR6 article-title: Simulation and experiment of cylinder shell structure dropping into water based on fluid structure interaction[J] publication-title: Journal of Beijing University of Aeronautics and Astronautics contributor: fullname: Zhang – volume: 190 start-page: 659 issue: 5–7 year: 2000 end-page: 675 ident: CR12 article-title: ALE formulation for fluid-structure interaction problems[J] publication-title: Computer Methods in Applied Mechanics and Engineering doi: 10.1016/S0045-7825(99)00432-6 contributor: fullname: Lewin – volume: 31 start-page: 509 issue: 3 year: 1994 ident: 2305637_CR3 publication-title: Spacecraft Rockets doi: 10.2514/3.26468 contributor: fullname: J R Brooks – volume: 18 start-page: 104 issue: 1 year: 2003 ident: 2305637_CR7 publication-title: Journal of Hydrodynamics, Ser. A contributor: fullname: H Sun – volume: 14 start-page: 227 issue: 3 year: 1974 ident: 2305637_CR4 publication-title: Journal of Computational Physics doi: 10.1016/0021-9991(74)90051-5 contributor: fullname: C W Hirt – volume: 21 start-page: 750 issue: 6 year: 2009 ident: 2305637_CR8 publication-title: Journal of Hydrodynamics doi: 10.1016/S1001-6058(08)60209-7 contributor: fullname: K Gong – volume: 29 start-page: 329 issue: 3 year: 1981 ident: 2305637_CR11 publication-title: Computer Methods in Applied Mechanics and Engineering doi: 10.1016/0045-7825(81)90049-9 contributor: fullname: T J R Hughes – volume: 18 start-page: 463 issue: 4 year: 2003 ident: 2305637_CR14 publication-title: Journal of Hydrodynamics, Ser. A contributor: fullname: B-z Yue – volume-title: 6th European LS-DYNA Users’Conference year: 2005 ident: 2305637_CR15 contributor: fullname: J Wang – volume-title: 10th International LS-DYNA Users Conference year: 2008 ident: 2305637_CR13 contributor: fullname: E J Karen – volume: 28 start-page: 718 issue: 5 year: 2010 ident: 2305637_CR9 publication-title: Journal of Northwestern Polytechnical University contributor: fullname: Z-y Wei – start-page: 181 volume-title: American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP year: 2004 ident: 2305637_CR10 contributor: fullname: M Souli – start-page: 19 volume-title: Civil Aircraft Design and Research year: 2007 ident: 2305637_CR1 contributor: fullname: S-d Wu – volume-title: 8th International LS-DYNA Users Conference Fluid/Structure year: 2004 ident: 2305637_CR5 contributor: fullname: B A Tutt – volume: 190 start-page: 659 issue: 5–7 year: 2000 ident: 2305637_CR12 publication-title: Computer Methods in Applied Mechanics and Engineering doi: 10.1016/S0045-7825(99)00432-6 contributor: fullname: M Souli – volume: 32 start-page: 1045 issue: 7 year: 2006 ident: 2305637_CR2 publication-title: International Journal of Impact Engineering doi: 10.1016/j.ijimpeng.2004.09.002 contributor: fullname: C M Seddon – volume: 33 start-page: 1117 issue: 9 year: 2007 ident: 2305637_CR6 publication-title: Journal of Beijing University of Aeronautics and Astronautics contributor: fullname: F Li |
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Snippet | Ditching is considered as one of the important aspects of safety performances of airplanes. It is related primarily with the fluid-solid interaction, whose... V216.5; Ditching is considered as one of the important aspects of safety performances of airplanes.It is related primarily with the fluid-solid... |
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SubjectTerms | Aircraft accidents Airplanes ALE方法 Arbitrary Lagrange-Euler (ALE) Computer simulation Ditching Engineering Engineering Fluid Dynamics finite element method fluid structure interaction Fluid-solid interactions Hydrology/Water Resources Mathematical analysis Mathematical models Numerical and Computational Physics Safety Simulation 安全性能 开沟 数值分析方法 数值模拟 水流 非线性有限元 飞机模型 |
Title | SIMULATION OF FLUID-SOLID INTERACTION ON WATER DITCHING OF AN AIRPLANE BY ALE METHOD |
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