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An Immersed interface method for simulating the interaction of a fluid with moving boundaries, (2006)

by Sheng Xu, Z Jane Wang
Venue:J. Comput. Phys.,
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Unconditionally stable discretizations of the immersed boundary equations

by Elijah P. Newren , Aaron L. Fogelson , Robert D. Guy , Robert M. Kirby , 2007
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Abstract - Cited by 41 (8 self) - Add to MetaCart
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Systematic derivation of jump conditions for the immersed interface method in three-dimensional flow simulation

by Sheng Xu, Z. Jane Wang - SIAM J. Sci. Comput
"... Abstract. In this paper, we systematically derive jump conditions for the immersed interface ..."
Abstract - Cited by 12 (3 self) - Add to MetaCart
Abstract. In this paper, we systematically derive jump conditions for the immersed interface
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...l submission of this paper, we have implemented and tested the IIM in two-dimensional flow simulations with jump conditions obtained from our theoretical derivation below. Please refer to Xu and Wang =-=[36]-=- for the full numerical implementation and the test results. The test results serve in part to verify our derivation in the current paper. We have also progressed on the development of a three-dimensi...

A second order virtual node method for elliptic problems with interfaces and . . .

by Jeffrey Lee Hellrung, Jr., Luming Wang , Eftychios Sifakis , Joseph M. Teran - JOURNAL OF COMPUTATIONAL PHYSICS , 2011
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Enhancing the immersed boundary method: Stability . . .

by Elijah Paul Newren , 2007
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Locally corrected semi-Lagrangian methods for Stokes flow with moving elastic interfaces

by J. Thomas Beale , John Strain , 2007
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A well-conditioned augmented system for solving Navier–Stokes equations in irregular domains

by Kazufumi Ito, et al. - JOURNAL OF COMPUTATIONAL PHYSICS , 2009
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A Velocity Decomposition Approach for Moving Interfaces in Viscous Fluids

by J. Thomas Beale, Anita T. Layton
"... We present a second-order accurate method for computing the coupled motion of a viscous fluid and an elastic material interface with zero thickness. The fluid flow is described by the Navier-Stokes equations, with a singular force due to the stretching of the moving interface. We decompose the veloc ..."
Abstract - Cited by 3 (2 self) - Add to MetaCart
We present a second-order accurate method for computing the coupled motion of a viscous fluid and an elastic material interface with zero thickness. The fluid flow is described by the Navier-Stokes equations, with a singular force due to the stretching of the moving interface. We decompose the velocity into a “Stokes ” part and a “regular ” part. The first part is determined by the Stokes equations and the singular interfacial force. The Stokes solution is obtained using the immersed interface method, which gives second-order accurate values by incorporating known jumps for the solution and its derivatives into a finite difference method. The regular part of the velocity is given by the Navier-Stokes equations with a body force resulting from the Stokes part. The regular velocity is obtained using a time-stepping method that combines the semi-Lagrangian method with the backward difference formula. Because the body force is continuous, jump conditions are not necessary. For problems with stiff boundary forces, the decomposition approach can be combined with fractional time-stepping, using a smaller time step to advance the interface quickly by Stokes flow, with the velocity computed using boundary integrals. The small time steps maintain numerical stability, while the overall solution is updated on a larger time step to reduce computational cost.
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...first expresses the jumps in the solution and its derivatives in terms of the boundary force and its derivatives, and then incorporates these jumps into a finite difference scheme as correction terms =-=[16,19,32]-=-. This method was first applied to the Stokes equations [16], the simplified model at zero Reynolds number in which acceleration and advection are neglected. The Stokes equations, (11) and (12) below,...

A Second Order Virtual Node Algorithm for Stokes Flow Problems with Interfacial Forces and Discontinuous Material Properties

by Diego C. Assêncio, Joseph M. Teran B
"... We present a numerical method for the solution of the Stokes equations that handles interfacial discontinuities due to both singular forces and discontinuous fluid properties such as viscosity and density. The discretization couples a Lagrangian representation of the material interface with an Euler ..."
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We present a numerical method for the solution of the Stokes equations that handles interfacial discontinuities due to both singular forces and discontinuous fluid properties such as viscosity and density. The discretization couples a Lagrangian representation of the material interface with an Eulerian representation of the fluid velocity and pressure. The method is efficient, easy to implement and yields discretely divergence-free velocities that are second order accurate. No knowledge of the jumps on the fluid variables and their derivatives is required along the interface. We discretize the equations using an embedded approach on a uniform MAC grid employing virtual nodes and duplicated cells at the interfaces. These additional degrees of freedom allow for accurate resolution of discontinuities in the fluid stress at the material interface but require a Lagrange multiplier term to enforce continuity of the fluid velocity. We provide a novel discretization of this term that accurately resolves the constant pressure null modes. We show that the accurate resolution of these modes accelerates the overall speed of our simulations. Interfaces are represented with a hybrid Lagrangian/level set method. The discrete coupled equations for the velocity, pressure and Lagrange multipliers are in the form of a symmetric KKT system. Numerical results indicate second order accuracy for the velocities and first order accuracy for the pressure (in L ∞).
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... interfacial discontinuities in the pressure, the velocities and their derivatives in a sharp manner. The IIM has been used in many fluid flow problems including interface and rigid boundary problems =-=[12, 19, 20, 21]-=-, Hele-Shaw flow [22] and also problems in which the viscosity is discontinuous across the interfaces [23, 24, 25]. Arbitrarily high orders of accuracy have been achieved [26, 27]. The method is consi...

1 A High-Order Cut-Cell Method for Numerical Simulation of Hypersonic-Boundary Transition with Arbitrary Surface Roughness

by Le Duan, Xiaowen Wang, Xiaolin Zhong
"... Hypersonic boundary-layer transition can be affected significantly by surface roughness. Many important mechanisms which involve transition induced by arbitrary roughness are not well understood. In this paper, we propose a new high-order cut cell method which combined the non-uniform finite differe ..."
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Hypersonic boundary-layer transition can be affected significantly by surface roughness. Many important mechanisms which involve transition induced by arbitrary roughness are not well understood. In this paper, we propose a new high-order cut cell method which combined the non-uniform finite difference method for discrete points near the curvilinear boundary and shock-fitting method for the bow shock. The receptivity process induced by interaction of Mach 5.92 flow over flat plate under the combination effect of two-dimensional surface roughness and blow-suction is investigated. Both steady state solutions and unsteady solutions have been obtained by using the new method. For steady flow with roughness, there is significant change inside the boundary layer with flow separation before and after the roughness element. For unsteady flow, the results for flow instability induced by both blow-suction slot and roughness are obtained and analyzed by Linear Stability Theory (LST). These results show that the roughness element with height to be half the boundary layer thickness may delay the hypersonic transition. I.
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...j j u q jjk k = ss (4)sIn this paper, only perfect-gas hypersonic flow is considered, i.e., p RT= (5) 1( ) 2 e C T u uv k k= +s(6) ( ) u uu ji k ij ijx x xj i k µ = + + =-=(7)-=- T q kj x j = (8) where R is the gas constant. The specific heats Cv are assumed to be constants with a given ratio of specific heats . The viscosity coefficient µ can be calculated by Sutherla...

A Second Order Virtual Node Method for Poisson Interface Problems on Irregular Domains

by Jacob Bedrossian, James H. Von Brechta, Siwei Zhua, Eftychios Sifakisa, Joseph M. Terana
"... We present a second order accurate, geometrically flexible and easy to implement method for solving the variable coefficient Poisson equation with interfacial discontinuities on an irregular domain. We discretize the equations using an embedded approach on a uniform Cartesian grid employing virtual ..."
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We present a second order accurate, geometrically flexible and easy to implement method for solving the variable coefficient Poisson equation with interfacial discontinuities on an irregular domain. We discretize the equations using an embedded approach on a uniform Cartesian grid employing virtual nodes at interfaces and boundaries. A variational method is used to define numerical stencils near these special virtual nodes and a Lagrange multiplier approach is used to enforce jump conditions and Dirichlet boundary conditions. Our combination of these two aspects yields a symmetric positive definite discretization. In the general case, we obtain the standard 5-point stencil away from the interface. For the specific case of interface problems with continuous coefficients, we present a discontinuity removal technique that admits use of the standard 5-point finite difference stencil everywhere in the domain. Numerical experiments indicate second order accuracy in L∞.
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... LeVeque and Li first proposed the IIM for approximating elliptic interface problems in [16] and the term now applies to a widely researched and extensively applied class of finite difference methods =-=[17, 18, 19, 20, 21, 22, 23]-=-. See [15] and the references therein for a complete exposition of the method and its 2 numerous applications, and [24] for justification of the general IIM approach. Using generalized Taylor expansio...

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