Slow Crack Growth of Germanium Jon Salem NASA GRC ICACC, January - - PowerPoint PPT Presentation

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Slow Crack Growth of Germanium Jon Salem NASA GRC ICACC, January - - PowerPoint PPT Presentation

https://ntrs.nasa.gov/search.jsp?R=20160010277 2018-04-24T03:01:31+00:00Z National Aeronautics and Space Administration Slow Crack Growth of Germanium Jon Salem NASA GRC ICACC, January 2016 www.nasa.gov 1 National Aeronautics and Space


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Slow Crack Growth of Germanium

Jon Salem NASA GRC ICACC, January 2016

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https://ntrs.nasa.gov/search.jsp?R=20160010277 2018-04-24T03:01:31+00:00Z

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Germanium

  • Good electromagnetic transmission in 2-15 μm
  • range. Specialty window material:

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Germanium

  • Brittle transition metal.
  • Relatively soft.
  • Behaves like a soft, brittle ceramic.
  • Stress corrosion cracking?
  • What is the fracture toughness?

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Material

  • Single crystal beams
  • Coarse gained disks (2” & 5”Φ):
  • Variable grain structure – not ideal for testing.

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25 mm

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Anisotropy

  • Anisotropy factor A* measures relative magnitude of

elastic anisotropy exhibited by a crystal. A* = 0 for isotropic materials, A* = 0 to 1 for many single crystals.

  • Relatively low. Running mechanical test on off-axis

planes is problematic if the anisotropy is large.

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Total Anisotropy Factor (Ac

*+As *)

5 10 15 20 25

Approximate Stress/Series Stress (Plate Center)

0.98 1.00 1.02 1.04 1.06 1.08

Tetragonal and Trigonal Materials, {010}

BaTiO3 In Sn TiO2 Sapphire Quartz

Anisotropy Factor A*

2 4 6 8 10 12 14 16 18

Approximate Stress/Series Stress (Plate Center)

1.00 1.02 1.04 1.06 1.08 1.10

Cubic materials, {100} NiAl -SiC GaP Ge Si MgO Diamond

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  • E<111> = 154.8 ± 0.9 GPa
  • E<110> = 138.3 ± 0.2
  • E<100> = 103.1 ± 0.6
  • Epoly = 131, vpoly = 0.21

Young’s Modulus

  • impulse excitation -

Ge McSkimin Bogardus McSkimin Mason Average NASA % Diff. Young’s Modulus (GPa) E<100> =

  • 104. 4

102.0 102.2 103.7 103.1 103.1 0.0% E<110> = 138.7 136.7 137.0 138.0 137.6 138.3 0.5% E<111> = 155.8 154.2 154.5 155.1 154.9 154.8

  • 0.1%

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}

Aggregate Constants GPa E v Voigt 135 0.20 Hashin 133 0.21 Shtrikman 132 0.21 Reuss 129 0.21

  • Well oriented germanium….
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Procedure

  • Fracture Toughness -
  • Three standard test methods (C1421):
  • Different crack size
  • Different crack formation history
  • Different effort

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W B ao a3 a2 a1 a1 a 2c

1= a1 /W o= ao /W =( a1+a2+a3) /3W

h Remove 4.5h to 5h

Precracked Beam (SEPB) Chevron Notch Beam (CNB) Surface Crack Flexure

(SCF)

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Loading Configuration

  • Fracture Toughness -

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  • Relatively simple fixtures: test frame, load cell, recording device.

SUPPORT ROD PUSH ROD

BALL

TEST SPECIMEN

Strain Gage Displacement Transducer

So Si

Si B So

5 10 15 20 25 30 35 40 50 100 150 200 250 300 350 400 Force (N) Backface Strain (µ m/m)

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Fracture Toughness

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  • Essentially the same on all planes
  • KIscf{jkl} = 0.74 ± 0.02 MPam
  • KIpb{100, 110} = 0.68 ± 0.04 MPam
  • ~10% difference between SCF and SEPB. Plasticity?
  • Practical value of KI{jkl} = 0.70 ± 0.02 MPam.

Method {100} {110} {111} SEPB 0.68 ± 0.04 0.68 ± 0.01 < 0.74 SCF 0.74 ± 0.02 0.74 ± 0.02 0.74 ± 0.02 CNB

In progress In progress In progress

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SCF Precracks

» {100} exhibit cathedral Wallner lines. » The most planar surface occurs on the {110}. » {111} tends to exhibit cleavage steps. » Secondary orientation was not fixed.

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{110}

<100>

{100}

<100>

{111}

<110> Precrack

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Cathedral Orientation

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<100> <110>

  • Peak of cathedral corresponds to the <100> {100}.

{100}

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0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1 2 3 4

Fracture Toughness, MPam L/t

Data of Jaccodine Cut off

KI{111} Data of Jaccodine

  • Reported an energy equivalent value of 0.55 MPam.
  • Used DCB w/ fracture mechanics solution that did not

include L/t effects.

  • Reanalysis gives KI{111} = 0.72 ± 0.05 MPam (6) w/

trend toward 0.67 MPam:

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 Engineering value ~0.68 MPam for low index planes

R.J. Jaccodine, “Surface Energy of Germanium and Silicon,” J. Electrochemical Soc., Vol. 110, No. 6, June, 1963, pp. 524- 527.

Valid range

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Strength Testing

  • Constant Stress Rate Tests

(5 MPa/s)

  • Biaxial Flexure ring-on-ring (ROR)
  • ~400 grit as-ground surfaces in

distilled, deionized water

  • ~Polished surface in lab air

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ASTM C1499

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Fracture Strength & Weibull Statistics

  • Polished m = 6; ground m = 9; spurious damage m = 4.
  • Scale effect evident: 168 vs 215 MPa.
  • Strength of 235 MPa is predicted vs 215 MPa (10%).

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θ m #/S

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Biaxial Fracture Patterns (polished)

  • Repetitive pattern that makes fractography difficult:

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Fracture Path

  • ground disk -

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Grinding Crack

#14-3, 36.1 MPa

Grain Boundary Grinding Lay Grinding Lay 8 mm Grain Boundary Grinding Crack

(#15-2)

  • Crack initiated at a grinding scratch.
  • Transited to a low index planes.
  • Deflected at a grain boundary.

25 mm

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  • Crack initiated from a semi-elliptical crack emanating

from a scratch.

  • Turned onto the {111} plane:
  • Opportunity to estimate the fracture toughness!
  • KI{hkl} = 0.73 MPa√m.
  • Why did the crack turn?

Fracture Path in a Polished ROR Disk

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9o from {110}

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Preferred Fracture Plane

  • The fracture toughness on low index planes is similar, so why is

the {111} the preferred propagation plane?

  • The {111} is the stiffest direction, and stiff directions exhibit high

stresses under strain controlled situations……

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Stress, MPa

0 10 20 30 40 50 60 70 80 90 100 10 20 30 40 50 60 70 80 90 100

Stress, MPa

Tangential Stress, r/Rs = 0.2 Radial Stress, r/Rs = 0.2 Tangential Stress, r/Rs = 0.8 Radial Stress, r/Rs = 0.8 <100> <110> <111> Isotropic

{110}

But, for a pressurized plate, the stress concentrations are not exhibited. Stress concentration where the load ring intersection the stiff direction.

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Fracture Toughness

– semi-elliptical cracks on high index planes -

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  • For polished specimens, KI = 0.77 ± 0.04 MPa√m (0.73-0.83).
  • For grinding cracks, KI = 0.87 ± 0.04 MPa√m (0.80 – 0.90).
  • Higher due to random orientation and transition to {111}.
  • Caveat: local stress not precisely know…..
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Slow Crack Growth

  • Experimental Approach -
  • Constant Stress Rate Testing “dynamic fatigue”
  • ASTM C1368
  • Strength based approach with advantages & disadvantages:
  • rapid test; simple geometry
  • samples the inherent, small flaws
  • statistical scatter (many specimens needed)
  • averaging of fatigue regions

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Experimental Procedure

  • Constant Stress Rate Tests

(5 to 5 x 10-4 MPa/s)

  • Biaxial Flexure (Ring-on-ring)
  • Distilled, deionized water
  • ~400 grit as-ground surfaces
  • ~10 tests per stress rate
  • ~40 tests

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Slow Crack Growth Analysis

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  • Parameter extraction via regression:

 

 

 

1 1 2

1

 

 

n n i f

n B    

   

2 2 2 2

2 2 2 2

   

n Y A K n AY K B

* Ic n Ic

  • Crack growth function:
  • Constant stress rate testing:

] K K [ A AK = dt da = v

n IC I n I

* 

D log log 1 n 1 log

10 10 f 10

     

 

 

2 n i 10 10

1 n B log 1 n 1 D log

   

(Slope ) (Intercept )

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Constant Stress Rate Curve

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  • Still some scatter.
  • Medians clarify the trend.
  • Slope is negative to zero; n > 100, no measurable SCG.

Ge

Russian Silica, Water Quartz-silica, water Corning 7980, water .

Stress Rate, , MPa/s 0.0001 0.001 0.01 0.1 1 10 100

Strength, Sf , MPa

20 30 40 50 60 80 100

Medians Water

Tosoh Fused Silica

Russian Silica, Water Quartz-silica, water Corning 7980, water .

Stress Rate, , MPa/s 0.001 0.01 0.1 1 10 100

Strength, Sf , MPa

20 30 40 50 60 70 80 10 100

Inert Strength Water

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Summary and Conclusions

  • Ge exhibits similar fracture toughness of KI = 0.68 ±

0.02 MPa√m on low index planes. Lower than Si!

  • Randomly oriented cracks exhibit higher apparent

toughness, but turn and propagate on the stiff {111} directions due to higher stresses (??)…..FEA.

  • Natural cleavage plane appears to be the {110}.
  • Weibull modulus varies from m = 4 (spurious) to m =

9 (ground).

  • Strength varies from Sf = 40 MPa (ground) to 160

MPa (polished).

  • Ge exhibits a Weibull scale effect, but does not

exhibit measurable SCG.

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Summary and Conclusions

  • Aggregate, polycrystalline Yong’s modulus and

Poisson’s ratio are Epoly = 131 GPa, vpoly = 0.21.

  • ROR loading results in stress concentrations at the

stiff directions of single crystals.

  • From a stress state point-of-view, a lower strength is

measurement is expected………

  • However, from an effective area perspective, a high

strength should be measured.

  • POR maybe a better test method, but more effort.

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Acknowledgements

  • Thanks to Terry McCue for SEM fractography.
  • Thanks to Rick Rogers for x-ray diffraction.
  • Thanks to Penni Dalton for funding & reviews.

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