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FE Post Processing • Plotting • Campbell Diagram • Goodman Diagram • Fracture • Yield • Principal Stress

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FE Post Processing. Plotting Campbell Diagram Goodman Diagram Fracture Yield Principal Stress. Post Processing plots. Deformed Shape Plot. Contour Plots. History Plot. Invert Colors for Hard Copies. Campbell Diagrams. Campbell Diagram. Probabilistic Campbell Diagram. - PowerPoint PPT Presentation

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Page 1: FE Post Processing

FE Post Processing

• Plotting• Campbell Diagram• Goodman Diagram• Fracture• Yield• Principal Stress

Page 2: FE Post Processing

POST PROCESSING PLOTS

Page 3: FE Post Processing

Deformed Shape Plot

Page 4: FE Post Processing

Contour Plots

Page 5: FE Post Processing

History Plot

Page 6: FE Post Processing

Invert Colors for Hard CopiesInvert Colors for Hard Copies

Page 7: FE Post Processing

CAMPBELL DIAGRAMS

Page 8: FE Post Processing

Campbell Diagram

0

500

1000

1500

2000

2500

3000

3500

0 2000 4000 6000 8000 10000 12000 14000

Fre

qu

en

cy -

Hz

Rotation Rate - RPM

Mode 1

Mode 2

Mode 3

EO: 1

EO: 3

EO: 6

EO: 10

EO: 11

EO: 12

EO: 15

Idle

Red Line

Page 9: FE Post Processing

Probabilistic Campbell Diagram

0

500

1000

1500

2000

2500

3000

3500

0 2000 4000 6000 8000 10000 12000 14000

Fre

qu

en

cy -

Hz

Rotation Rate - RPM

Mode 1

Mode 2

Mode 3

EO: 1

EO: 3

EO: 6

EO: 10

EO: 11

EO: 12

EO: 15

Idle

Red Line

Page 10: FE Post Processing

GOODMAN DIAGRAMS

Page 11: FE Post Processing

Inputs Include

• Material:– Ultimate tensile strength, – Yield stress – 0.2%,– High cycle fatigue strength,

• Loads– Steady stress,– Vibratory,

• Half amplitude, zero-peak, • Full amplitude, peak-peak,

UTS

Y

1R

0

pp

Page 12: FE Post Processing

Load Inputs

max

min

R

Page 13: FE Post Processing

HCF Test Data

• Fit R=-1 data– For example:

• Pick number of cycles to failure: Nf

• Solve for corresponding half-amplitude stress:

110 /log Rf BAN

1R

Page 14: FE Post Processing

Goodman DiagramMaterial Inputs

110 /log Rf BAN

Page 15: FE Post Processing

My Choice

Page 16: FE Post Processing

FRACTURE MECHANICS

Page 17: FE Post Processing

Fracture Modes

Page 18: FE Post Processing

Stress Intensity FactorMode I

Stresses near crack tip are singular and vary as the inverse square root of distance from crack tipKI is the stress intensity factor

Page 19: FE Post Processing

Fracture – ¼ Points

Page 20: FE Post Processing

Modeling Cracks

Page 21: FE Post Processing

VON MISES STRESS&

PLASTIC YIELDING

Page 22: FE Post Processing

Von Mises Stress

zzyzxz

yzyyxy

xzxyxx

is the stress tensor

3zzyyxxp

is the equivalent hydrostatic pressure

p

p

p

sss

sss

sss

s

zzyzxz

yzyyxy

xzxyxx

zzyzxz

yzyyxy

xzxyxx

is the deviatoric stress

Page 23: FE Post Processing

Invariants of Stress

• Invariants do not change values when coordinate system is rotated.

• The first invariant of the stress is

• The second invariant of the deviatoric stress is

• The third invariant of the deviatoric stress is the determinant.

.31 pI zzyyxx

.2

1 2222222222 zzyzxzyzyyxyxzxyxx sssssssssJ

Page 24: FE Post Processing

Uniaxial Tension

000

000

00y

33yzzyyxxp

y

y

yp

zzyzxz

yzyyxy

xzxyxx

p

p

p

s

3

100

03

10

003

2

22222 3

1

9

1

9

1

9

4

2

1yyyyJ

:yield stressy

Page 25: FE Post Processing

Equivalent Mises Stress

• Yielding occurs when

• Or when equivalent stress

• When yielding occurs

• Stress ratio is

03

1 22 yJ

23JvM

yvM

yvM /

Page 26: FE Post Processing

PRINCIPAL STRESSES

Page 27: FE Post Processing

Principal Stresses

• Eigenvalues of stress tensor (matrix) are principal stresses– All values are real– Order is 1:maximum, 2: intermediate, 3:minimum

• Associated eigenvectors are normal to face• Use maximum principal stress for fracture

1

2

3

x

y

z

Page 28: FE Post Processing

STRESS CONTOURS

Page 29: FE Post Processing

Ansys Stress Contour Plots

Page 30: FE Post Processing

FE Post Processing• Plotting

– Includes displaced, contour, and scatter plots• Campbell Diagram

– Finds important resonances• Goodman Diagram

– Predicts high cycle fatigue life• Fracture

– Indicates failure due to crack propagation• Yield

– Establishes yield through the use of equivalent (Mises) stress• Principal Stress

– Aids in determining failure due to presence of flaws