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Static Analysis

MESH:

Entity Size

Nodes 86579

Elements 51858

ELEMENT TYPE:

Connectivity Statistics

TE10 51858 ( 100.00% )

ELEMENT QUALITY:

Criterion Good Poor Bad Worst Average

Stretch 51808 ( 99.90% ) 50 ( 0.10% ) 0 ( 0.00% ) 0.232 0.632

Aspect Ratio 47667 ( 91.92% ) 4180 ( 8.06% ) 11 ( 0.02% ) 5.371 1.906

Materials.1

Material Aluminium

Young's modulus 7e+010N_m2

Poisson's ratio 0.346

Density 2710kg_m3

Coefficient of thermal expansion 2.36e-005_Kdeg

Yield strength 9.5e+007N_m2

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Static Case

Boundary Conditions

Figure 1

STRUCTURE Computation

Number of nodes : 86579

Number of elements : 51858

Number of D.O.F. : 259737

Number of Contact relations : 0

Number of Kinematic relations : 0

Parabolic tetrahedron : 51858

RESTRAINT Computation

Name: Restraints.1

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Number of S.P.C : 5172

LOAD Computation

Name: Loads.1

Applied load resultant :

Fx = -5 . 085e-007 N

Fy = 1 . 494e-007 N

Fz = -4 . 000e+004 N

Mx = -2 . 661e+003 Nxm

My = -4 . 064e+003 Nxm

Mz = -2 . 448e-008 Nxm

STIFFNESS Computation

Number of lines : 259737

Number of coefficients : 9959619

Number of blocks : 20

Maximum number of coefficients per bloc : 500000

Total matrix size : 114 . 97 Mb

SINGULARITY Computation

Restraint: Restraints.1

Number of local singularities : 0

Number of singularities in translation : 0

Number of singularities in rotation : 0

Generated constraint type : MPC

CONSTRAINT Computation

Restraint: Restraints.1

Number of constraints : 5172

Number of coefficients : 0

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Number of factorized constraints : 5172

Number of coefficients : 0

Number of deferred constraints : 0

FACTORIZED Computation

Method : SPARSE

Number of factorized degrees : 254565

Number of supernodes : 5962

Number of overhead indices : 1226241

Number of coefficients : 135783783

Maximum front width : 4230

Maximum front size : 8948565

Size of the factorized matrix (Mb) : 1035 . 95

Number of blocks : 136

Number of Mflops for factorization : 2 . 206e+005

Number of Mflops for solve : 5 . 444e+002

Minimum relative pivot : 5 . 269e-002

Minimum and maximum pivot

Value Dof Node x (in) y (in) z (in)

3.5674e+007 Tx 67400 -2.8905e+000 1.8697e+000 2.2905e+000

5.7599e+009 Ty 45492 5.7372e-001 1.3300e+000 -2.9409e+000

Minimum pivot

Value Dof Node x (in) y (in) z (in)

3.8964e+007 Tx 64249 3.0741e-001 2.0328e+000 -5.5334e+000

4.0496e+007 Tz 82214 -2.2219e+000 8.4744e-001 4.9227e-001

4.1066e+007 Tx 59256 2.1204e-001 -1.5995e+000 6.8684e+000

4.1323e+007 Tx 74690 -8.6636e+000 -4.6436e-001 -3.9586e+000

4.1986e+007 Tz 74816 -5.1137e+000 2.1182e+000 8.3112e+000

4.5861e+007 Tx 58028 -3.0000e+000 -1.1382e+000 8.7661e+000

4.9121e+007 Tz 74923 -5.1290e+000 3.1702e+000 1.0981e+001

5.3023e+007 Ty 69161 -4.7292e+000 6.3331e-001 -7.1148e+000

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5.5193e+007 Ty 82214 -2.2219e+000 8.4744e-001 4.9227e-001

Translational pivot distribution

Value Percentage

10.E7 --> 10.E8 1.1746e-001

10.E8 --> 10.E9 4.8132e+001

10.E9 --> 10.E10 5.1751e+001

DIRECT METHOD Computation

Name: Static Case Solution.1

Restraint: Restraints.1

Load: Loads.1

Strain Energy : 1.084e+000 J

Equilibrium

Components  Applied

Forces  Reactions Residual

  RelativeMagnitude Error

Fx (N) -5.0850e-007 5.0929e-007 7.8302e-010 6.7043e-013

Fy (N) 1.4943e-007 -1.5068e-007 -1.2477e-009 1.0683e-012

Fz (N) -4.0000e+004 4.0000e+004 1.3169e-009 1.1276e-012

Mx (Nxm) -2.6611e+003 2.6611e+003 2.8149e-010 8.5484e-013

My (Nxm) -4.0640e+003 4.0640e+003 3.7926e-010 1.1518e-012

Mz (Nxm) -2.4480e-008 2.4561e-008 8.1364e-011 2.4709e-013

Static Case Solution.1 - Deformed mesh.2

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Figure 2

On deformed mesh ---- On boundary ---- Over all the model

Static Case Solution.1 - Von Mises stress (nodal values).2

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Figure 3

3D elements: : Components: : All

On deformed mesh ---- On boundary ---- Over all the model

Static Case Solution.1 - Deformed mesh.1

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Figure 4

On deformed mesh ---- On boundary ---- Over all the model

Static Case Solution.1 - Von Mises stress (nodal values).1

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Figure 5

3D elements: : Components: : All

On deformed mesh ---- On boundary ---- Over all the model

Static Case Solution.1 - Translational displacement vector.1

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Figure 6

3D elements: : Components: : All

On deformed mesh ---- On boundary ---- Over all the model

Static Case Solution.1 - Estimated local error.1

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Figure 7

3D elements: : Components: : All

On all Elements ---- Over all the model

Global Sensors

Sensor Name Sensor Value

Energy 1.084J

Global Error Rate (%) 12.810677528

Analysis file:///C:/Users/Alex/Desktop/Indexer/1600indx report/i