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Featured researches published by M.J. Caton.


51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th | 2010

Understanding Materials Uncertainty for Prognosis of Advanced Turbine Engine Materials

James M. Larsen; M.J. Caton; Sushant K. Jha; Andrew H. Rosenberger; Reji John; Dennis J. Buchanan; Jay R. Jira; Patrick J. Golden

Abstract : Materials damage prognosis offers the opportunity to revolutionize life management of advanced materials and structures through a combination of improved state awareness, physically based predictive models of damage and failure, and autonomic reasoning. Historically, lifetime and reliability limits for advanced fracture-critical turbine engine materials have been based on expected worst-case total life under fatigue. Recent findings in a variety of advanced propulsion alloys indicate that the life-limiting mechanisms are typically dominated by the growth of damage that begins at the scale of key microstructural features. Such behavior provides new avenues for management and reduction of uncertainty in prognosis capability under conditions that depend on damage tolerance. To examine a range of sources of uncertainty in behavior and models of such behavior, this paper explores the following topics: (1) Duality in Fatigue, (2) Relaxation of Surface Residual Stresses in Laboratory Specimens, (3) Relaxation of Bulk Residual Stresses in Components, (4) Nonlinear Acoustic Parameter for the Detection of Precursor Fatigue Damage, (5) Elevated Temperature Fretting Fatigue, (6) Crack Growth under Spin Pit Environments, and (7) Crack Growth Under Variable Amplitude High Cycle Fatigue (HCF) Loading. Based on the findings, we outline avenues for further technology development, maturation, validation, and transition of mechanistically based models that have the potential to reduce predictive uncertainty for current and future materials.


Materials Science and Engineering A-structural Materials Properties Microstructure and Processing | 2007

A new paradigm of fatigue variability behavior and implications for life prediction

S.K. Jha; M.J. Caton; J. M. Larsen


International Journal of Fatigue | 2012

Stress ratio effects on small fatigue crack growth in Ti–6Al–4V

M.J. Caton; Reji John; W.J. Porter; M.E. Burba


Superalloys | 2008

MEAN VS. LIFE-LIMITING FATIGUE BEHAVIOR OF A NICKEL-BASED SUPERALLOY

Sushant K. Jha; M.J. Caton; J. M. Larsen


Superalloys | 2004

Development of ultrasonic fatigue for rapid, high temperature fatigue studies in turbine engine materials

Amit Shyam; Christopher J. Torbet; Sushant K. Jha; J. M. Larsen; M.J. Caton; Christopher J. Szczepanski; Tresa M. Pollock; J. W. Jones


International Journal of Fatigue | 2010

Small fatigue crack growth and failure mode transitions in a Ni-base superalloy at elevated temperature

M.J. Caton; S.K. Jha


Superalloys | 2004

Divergence of Mechanisms and the Effect on the Fatigue LIfe Variablity of Rene' 88 DT

M.J. Caton; Sushant K. Jha; Andrew H. Rosenberger; J. M. Larsen


Procedia Engineering | 2010

Stability of Shot Peen Residual Stresses in IN100 Subjected to Creep and Fatigue Loading

Reji John; Dennis J. Buchanan; M.J. Caton; Sushant K. Jha


Superalloys | 2008

Microstructural Conditions Contributing to Fatigue Variability in P/M Nickel-Base Superalloys (Preprint)

W J Porter; K Li; M.J. Caton; Sushant K. Jha; B B Bartha; J M Larsen


Experimental Mechanics | 2015

Developing the Capability to Monitor Small Fatigue Crack Growth Under Elevated Temperature, Ultra-High Vacuum Conditions

B. T. Gockel; M.J. Caton; S. K. Jha; C. J. Szczepanski; A. H. Rosenberger; M. E. Burba

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Sushant K. Jha

Wright-Patterson Air Force Base

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Reji John

Air Force Research Laboratory

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Amit Shyam

Oak Ridge National Laboratory

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Andrew H. Rosenberger

Wright-Patterson Air Force Base

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Dennis J. Buchanan

Air Force Research Laboratory

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J. W. Jones

University of Michigan

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A. H. Rosenberger

Air Force Research Laboratory

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C. J. Szczepanski

Air Force Research Laboratory

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