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Development of A Life Prediction Scheme For the Assessment of Fatigue Performance of Composite Infra

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Employ a representative volume ... Volume. Critical. Element. Subcritical ... upon tensor strength and stresses; use this failure function for calculations ... – PowerPoint PPT presentation

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Title: Development of A Life Prediction Scheme For the Assessment of Fatigue Performance of Composite Infra


1
Development of A Life Prediction Scheme For the
Assessment ofFatigue Performance of Composite
Infrastractures
  • S. W. Case1, J. J. Lesko1, and T. E. Cousins2
  • 1Department of Engineering Science and Mechanics
  • 2Via Department of Civil Engineering
  • Virginia Polytechnic Institute and State
    University
  • Blacksburg, VA 24061, USA

2
Outline
  • Motivation for the research
  • Modeling philosophy
  • Modeling predictions and comparison to data
  • Conclusions
  • Ongoing and future work

3
Composites infrastructure
  • Moisture(, n, t)
  • Stress(s, n, t)
  • UV(I, t)
  • Temperature(T, n)
  • Obstacles
  • Absence of design standards
  • Durability?
  • New material multiple combinations processing
    methods
  • Comfort, Experience Acceptance by the DOT

4
Infrastructure composites durability Approach
Field Investigations
Laboratory Experimentation
Durability Prediction
Durable designs design philosophies for 50-75
year design lives
5
Critical element model
  • Employ a representative volume
  • Define critical element so that failure of the
    critical element results in failure of the
    material
  • Remainder of the material make up subcritical
    elements--control stress redistribution
  • Define rate equations for each of the processes
    that govern material behavior

s
(t)
Critical
Element
Representative
Volume
Subcritical
Elements
6
The use of remaining strength as a state variable
  • Track remaining strength of the critical element
    during the fatigue process
  • Define a scalar failure function based upon
    tensor strength and stresses use this failure
    function for calculations
  • May include the effects of changing loading
    conditions
  • Can be directly validated experimentally, unlike
    Miners rule

Sult
Stress or Strength
Life Curve
t1
t2
Time
7
The use of remaining strength as a state variable
  • Track remaining strength of the critical element
    during the fatigue process
  • Define a scalar failure function based upon
    tensor strength and stresses use this failure
    function for calculations
  • May include the effects of changing loading
    conditions
  • Can be directly validated experimentally, unlike
    Miners rule

Residual Strength
8
The use of remaining strength as a state variable
  • Track remaining strength of the critical element
    during the fatigue process
  • Define a scalar failure function based upon
    tensor strength and stresses use this failure
    function for calculations
  • May include the effects of changing loading
    conditions
  • Can be directly validated experimentally, unlike
    Miners rule

Residual Strength
9
The use of remaining strength as a state variable
  • Track remaining strength of the critical element
    during the fatigue process
  • Define a scalar failure function based upon
    tensor strength and stresses use this failure
    function for calculations
  • May include the effects of changing loading
    conditions
  • Can be directly validated experimentally, unlike
    Miners rule

10
Mathematical representation
  • Define a failure criterion, Fa, and a remaining
    strength in terms of that failure criterion, Fr
  • Define a generalized time (for example n/N)
  • From kinetics we have the change in remaining
    strength over the interval
  • Fa is constant over
  • For the special case in which is equal to zero
  • Some possible choices for failure criteria
  • Maximum stress/strain
  • Tsai-Hill/Tsai-Wu

11
Mathematical representation
  • For step loading, introduce the concept of
    "pseudo-cycles" based on the idea of equivalent
    damage

12
Mathematical representation
  • Calculate change in remaining strength over the
    interval
  • Calculate number of cycles required for failure

13
Life prediction example (APC-2)
14
Life prediction exampleUnidirectional S-N data
(R0.05)
15
Life prediction exampleNotched quasi-isotropic
laminate (R-1)
16
Life prediction exampleNotched quasi-isotropic
laminate (R-1)
17
Conclusions
  • A life prediction method for composites based
    upon remaining strength has been developed.
    Features of the model are
  • Inclusion of sequence effects
  • Ability to combine effects (such as fatigue and
    stress rupture)
  • An example application has been considered

18
Ongoing/Future work
  • Developing and applying analysis techniques for
    composites typical of infrastructure (Phifer et
    al.)
  • Using results from in-service tests to guide and
    refine the modeling efforts

19
Acknowledgements
  • Federal Highway Administration Priority
    Technology Program
  • Virginia Transportation Research Council
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