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A meshless method for the Reissner-Mindlin plate equations based on - - PowerPoint PPT Presentation

A meshless method for the Reissner-Mindlin plate equations based on a stabilized mixed weak form using maximum-entropy basis functions J.S. Hale*, P.M. Baiz 11th September 2012 J.S. Hale 1 Mixed MaxEnt Method for Plates - ECCOMAS 2012


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A meshless method for the Reissner-Mindlin plate equations based on a stabilized mixed weak form using maximum-entropy basis functions

J.S. Hale*, P.M. Baiz

11th September 2012

J.S. Hale Mixed MaxEnt Method for Plates - ECCOMAS 2012 1

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Introduction

Aim of the research project

Develop a meshless method for the simulation of Reissner-Mindlin plates that is free of shear locking.

Figure : 6th free vibration mode of SSSS plate

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Existing Approaches (FE and Meshless)

◮ Reduced Integration (Many authors) ◮ Assumed Natural Strains (ANS) (eg. MITC elements, Bathe) ◮ Enhanced Assumed Strains (EAS) (Hughes, Simo etc.) ◮ Discrete Shear Gap Method (DSG) (Bletzinger, Bischoff, Ramm) ◮ Smoothed Conforming Nodal Integration (SCNI) (Wang and Chen) ◮ Matching Fields Method (Donning and Liu) ◮ Direct Application of Mixed Methods (Hale and Baiz)

The Connection

Many of these methods are based on, or have been shown to be equivalent to, mixed variational methods.

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Key Features of the Method

Weak Form

Design is based upon on a Stabilised Mixed Weak Form, like many successful approaches in the Finite Element literature.

Stabilised Mixed Weak Form (Brezzi and Arnold 1993, Boffi and Lovadina 1997)

ab(θ; η) + λαas(θ, z3; η, y3) + (γ, ∇y3 − η)L2 = f (y3) (1a) (∇z3 − θ, ψ)L2 − ¯ t2 λ(1 − α¯ t2)(γ; ψ)L2 = 0 (1b)

J.S. Hale Mixed MaxEnt Method for Plates - ECCOMAS 2012 4

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Key Features of the Method

Basis Functions

Uses (but is not limited to!) Maximum-Entropy Basis Functions which have a weak Kronecker-delta property. On convex node sets boundary conditions can be imposed directly.

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Key Features of the Method

Localised Projection Operator

Shear Stresses are eliminated on the ‘patch’ level using a localised projection operator which leaves a final system of equations in the displacement unknowns only.

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The Reissner-Mindlin Problem

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The Reissner-Mindlin Problem

Displacement Weak Form

Find (z3, θ) ∈ (V3 × R) such that for all (y3, η) ∈ (V3 × R):

  • Ω0

Lǫ(θ) : ǫ(η) dΩ + λ¯ t−2

  • Ω0

(∇z3 − θ) · (∇y3 − η) dΩ =

  • Ω0

gy3 dΩ (2)

  • r:

ab(θ; η) + λ¯ t−2as(θ, z3; η, y3) = f (y3) (3)

Locking Problem

Whilst this problem is always stable, it is poorly behaved in the thin-plate limit ¯ t → 0

J.S. Hale Mixed MaxEnt Method for Plates - ECCOMAS 2012 8

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Shear Locking

102 103

number of degrees of freedom

10−7 10−6

L2 error in z3

t = 0.002 t = 0.02 t = 0.2

J.S. Hale Mixed MaxEnt Method for Plates - ECCOMAS 2012 9

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Shear Locking

The Problem

Inability of the basis functions to represent the limiting Kirchhoff mode ∇z3 − η = 0 (4)

A solution?

Move to a mixed weak form

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Mixed Weak Form

Treat the shear stresses as an independent variational quantity: γ = λ¯ t−2(∇z3 − θ) ∈ S (5)

Mixed Weak Form

Find (z3, θ, γ) ∈ (V3 × R × S) such that for all (y3, η, ψ) ∈ (V3 × R × S): ab(θ; η) + (γ; ∇y3 − η)L2 = f (y3) (6a) (∇z3 − θ; ψ)L2 − ¯ t2 λ (γ; ψ)L2 = 0 (6b)

Stability Problem

Whilst this problem is well-posed in the thin-plate limit, ensuring stability is no longer straightforward

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Stabilised Mixed Weak Form

Displacement Formulation

Locking as ¯ t → 0

Mixed Formulation

Not necessarily stable

Solution

Combine the displacement and mixed formulation to retain the advantageous properties of both

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Stabilised Mixed Weak Form

Split the discrete shear term with a parameter 0 < α < ¯ t−2 that is independent of the plate thickness: as = αadisplacement + (¯ t−2 − α)amixed (7)

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Stabilised Mixed Weak Form

Mixed Weak Form

Find (z3, θ, γ) ∈ (V3 × R × S) such that for all (y3, η, ψ) ∈ (V3 × R × S): ab(θ; η) + (γ; ∇y3 − η)L2 = f (y3) (8a) (∇z3 − θ; ψ)L2 − ¯ t2 λ (γ; ψ)L2 = 0 (8b)

Stabilised Mixed Weak Form (Brezzi and Arnold 1993, Boffi and Lovadina 1997)

ab(θ; η) + λαas(θ, z3; η, y3) + (γ, ∇y3 − η)L2 = f (y3) (9a) (∇z3 − θ, ψ)L2 − ¯ t2 λ(1 − α¯ t2)(γ; ψ)L2 = 0 (9b)

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α independence

10−4 10−3 10−2 10−1

thickness ¯ t

10−3 10−2 10−1

eH1(z3)

α independence with fixed discretisation h = 1/8, α = 32.0

eH1 (z3) J.S. Hale Mixed MaxEnt Method for Plates - ECCOMAS 2012 15

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Eliminating the Stress Unknowns

◮ Find a (cheap) way of eliminating the extra unknowns

associated with the shear-stress variables γh = λ(1 − α¯ t2) ¯ t2 Πh(∇z3h − θh, ψh) (10)

Figure : The Projection Πh represents a softening of the energy associated with the shear term

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Eliminating the Stress Unknowns

◮ We use a version of a technique proposed by Ortiz, Puso and

Sukumar for the Incompressible-Elasticity/Stokes’ flow problem which they call the “Volume-Averaged Nodal Pressure” technique.

◮ A more general name might be the “Local Patch Projection”

technique.

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Eliminating the Stress Unknowns

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Eliminating the Stress Unknowns

For one component of shear (for simplicity): (z3,x −θ1, ψ13)L2 − ¯ t2 λ(1 − α¯ t2)(γ13; ψ13)L2 = 0 (11) Substitute in meshfree and FE basis, perform row-sum (mass-lumping) and rearrange to give nodal shear unknown for a node a. Integration is performed over local domain Ωa: γ13a =

N

  • i=1
  • Ωa Na {−φi

φi,x} dΩ

  • Ωa Na dΩ

φi z3i

  • (12)

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Choosing α

The dimensionally consistent choice for α is length−2. In the FE literature typically this paramemeter has been chosen as either h−1

  • r h−2 where h is the local mesh size.

Meshless methods

A sensible place to start would be ρ−2 where ρ is the local support size.

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2.4 2.6 2.8 3.0 3.2 3.4 3.6 log10(dim U) −2 −1 1 2 3 4 log10(α) α ∼ 1/ρ2 Convergence surface for eL2(z3) −4.0 −3.5 −3.0 −2.5 −2.0 −1.5 −1.0 −0.5 0.0

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2.4 2.6 2.8 3.0 3.2 3.4 3.6 log10(dim U) −2 −1 1 2 3 4 log10(α) α ∼ 1/ρ2 Convergence surface for eH1(z3) −3.0 −2.5 −2.0 −1.5 −1.0 −0.5 0.0

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Results - Convergence

102 103 104

dim U

10−5 10−4 10−3 10−2 10−1

e

Convergence of deflection in norms with α ∼ O(h−2)

eL2 (z3) eH1 (z3) J.S. Hale Mixed MaxEnt Method for Plates - ECCOMAS 2012 23

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Results - Surface Plots

Figure : Displacement z3h of SSSS plate on 12 × 12 node field + ‘bubbles’, t = 10−4, α = 120

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Results - Surface Plots

Figure : Rotation component θ1 of SSSS plate on 12 × 12 node field + ‘bubbles’, t = 10−4, α = 120

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Summary

A method:

◮ using (but not limited to) Maximum-Entropy basis functions

for the Reissner-Mindlin plate problem that is free of shear-locking

◮ based on a stabilised mixed weak form ◮ where secondary stress are eliminated from the system of

equations a priori using “Local Patch Projection” technique Possible future work:

◮ Extension to Naghdi Shell model ◮ Investigate locking-free PUM enriched methods

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Thanks for listening.

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LBB Stability Conditions

Theorem (LBB Stability)

The discretised mixed problem is uniquely solvable if there exists two positive constants αh and βh such that: ab(ηh; ηh) ≥ αhηh2

Rh

∀ηh ∈ Kh (13a) inf

ψh∈Sh

sup

(ηh,y3h)∈(Rh×V3h)

((∇y3h − ηh), ψh)L2 (ηhRh + y3hV3h)ψhS′

h

≥ βh (13b)

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LBB Stability Conditions

The Problem

◮ To satisfy the second condition 13b make displacement spaces

Rh × V3h ‘rich’ with respect to the shear space Sh

◮ If Rh × V3h is too ‘rich’ then the first condition 13a may fail

as Kh grows.

◮ Balancing these two competing requirements makes the

design of a stable formulation difficult.

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