Chapter 6 Introduction to Finite Element Analysis Flashcards

1
Q

FEM software tools

A
  1. CAD, standard parts, material database
  2. CAE: preprocessor, finite element solver, postprocessor
  3. CAD, CAM
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2
Q

3 types of error

A
  1. solution error (usually negligible)
  2. discretization error (how many domains do I need for a valid answer?)
  3. idealization error (is the model correct in terms of physics?)
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3
Q

classification of finite elements

A
  1. 1D, 2D, 3D
  2. linear, quadratic, cubic
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4
Q

1D elements

A

provide (usually) axial stiffness (e.g. stringers)

CROD, CBAR

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5
Q

2D elements

A

covering surfaces (e.g. skin)

CTRIA, CQUAD4

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6
Q

3D elements

A

e.g. interfaces of VTP and HTP, detailed finite element models

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7
Q

essential boundary condition

A

Dirichlet BC

directly imposed to a DOF (supports)

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8
Q

natural boundary condition

A

Neumann BC

loading

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9
Q

Direct Stiffness Method (DSM)

A

breakdown:
1. disconnection
2. localization
3. member (elements) formation

assembly and solution:
4. globalization
5. merge
6. application of BCs
7. solution
8. recovery of derived quantities

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10
Q

rules for assembly

A

compatibility: joint displacement of all members meeting at a joint must be the same

equilibrium: sum of forces by all members that meet at a joint must balance the external force applied to that joint

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11
Q

Tonti diagram of governing equations

A

given (problem data) (external):
1. prescribed end displacements
2. distributed axial load q(x)
3. prescribed end loads

unknowns (internal):
1. axial displacements u(x)
2. axial strains e(x)
3. axial dorce F(x)

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12
Q

minimum potential energy (MPE) principle

A

nature wants to stay at equilibrium

for conservative structural systems, of all the kinematically admissible deformations, those corresponding to the equilibrium state extremize (i.e., minimize or maximize) the total potential energy

if the extremum is a minimum, the equilibrium state is stable.

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13
Q

consistent nodal force vector

A

external loads are sometimes applied to a whole element (e.g. pressure), but in FEM the forces must be applied only on nodes, hence we “lump” the loads to the nodes

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14
Q

each node must be connected to […] stiffness values

A

each node must be connected to 6 stiffness values (each for one DOF), otherwise a singularity will occur

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15
Q

discretization error goes to zero when …

A

… when the number of finite elements goes to infinity

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16
Q

stress gradient and refinment

A

the higher the stress gradient, the more finite elements are required e.g. at the following positions: holes, cross-sectional changes, inner radii, in-plane bending