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McClung, R. C. (2005). "A Bibliography and
Abstracts on the Stability of Residual Stresses and Their Influence
on Fatigue." |
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Srivatsa, S. (2005). "Deformation Strain Needed
to Crack Hard Alpha Anomalies."
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Srivatsa, S. (2002). "Turbine Rotor Material
Design Task 2: Effect of Forging on Defect Morphology Phase
II Report."
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Woodfield, A. (2002). "Sensitivity of Ti-17 to
an Oxygen-Stabilized Hard Alpha."
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Southwest Research Institute, Allied Signal,
General Electric, Pratt & Whitney, Rolls-Royce Allison,
Scientific Forming Technologies (2000). Turbine Rotor Material Design, Phase 1
Final Report, FAA Grant 95-G-041, Federal Aviation Administration,
Washington, DC. Note: this file is very
large (86 MB)
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Articles and
Presentations | |
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Phase II Article List |
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Phase II Presentation
List |
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Phase I Article List |
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Phase I Presentation
List |
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| 2007 |
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Millwater, H.R. et
al. (2007). "Convergent zone-refinement method for risk
assessment of gas turbine disks subject to low-frequency
metallurgical defects," Journal of Engineering for Gas Turbine and
Power, Volume 129, pp.
827-835. |
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| 2006 |
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Millwater, H.R. and Osborn, R.W. (2006).
"Probabilistic sensitivities for fatigue analysis of turbine
engine disks," International Journal of Rotating
Machinery, Volume 2006, pp. 1-12. |
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Enright, M.P. and Huyse, L. (2006).
"Methodology for probabilistic life prediction of multiple anomaly
materials," AIAA Journal, 44(4), pp.
787-793. |
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Enright, M.P. et
al. (2006). "Adaptive optimal sampling methodology for
reliability prediction of series systems," AIAA Journal,
44(3), pp. 523-528. | |
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| 2005 |
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Enright, M.P. et
al. (2005). "Fracture mechanics-based probabilistic life
prediction of components with large numbers of inherent material
anomalies," Proceedings Ninth International
Conference on Structural Safety and Reliability (ICOSSAR), Rome,
Italy, June 19-23, pp. 601-607. |
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Enright, M.P. et
al. (2005). "A probabilistic framework for risk prediction of
engine components with inherent and induced material anomalies," Proceedings 50th ASME International Gas Turbine
& Aeroengine Technical Congress, Reno, NV, June 6-9, Paper
GT2005-68982. |
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Jameel, A. (2005). "Surface damage tolerance
analysis of a gas turbine engine rotor", Proceedings 50th ASME International Gas Turbine
& Aeroengine Technical Congress, Reno, NV, June 6-9, Paper
GT2005-68760. |
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Enright, M.P. et
al. (2005). "Methodology for probabilistic life prediction of
multiple anomaly materials," Proceedings of
the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and
Materials Conference, Austin, TX, April 18-21. |
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Momin, F.N. et al.
(2005). "Application of the generalized conditional expectation
method for enhancing probabilistic fatigue design code," Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC
Structures, Structural Dynamics, and Materials Conference,
Austin, TX, April 18-21. |
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Osborn, W. et al.
(2005). "Application of probabilistic sensitivities to probabilistic
fatigue analysis of gas turbine engine disks," Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC
Structures, Structural Dynamics, and Materials Conference,
Austin, TX, April 18-21. | |
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| 2004 |
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Momin, F.N. et al.
(2004). "Application of a Conditional Expectation Response Surface
Approach to Probabilistic Fatigue," 9th
ASCE Speciality Conference on Probabilistic Mechanics and
Structural Reliability, ASCE, Albuquerque, NM, July,
ASCE Paper PMC2004-204. |
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McClung, R.C. et
al. (2004). "Efficient fracture design for complex turbine
engine components," Proceedings, 49th
ASME International Gas Turbine & Aeroengine Technical
Congress, ASME, Vienna, Austria, June 14-17, ASME Paper
GT2004-53323. |
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Enright, M.P. et
al. (2004). "Adaptive Optimal Sampling Methodology for
Zone-Based Probabilistic Life Prediction," Proceedings of the 45th AIAA/ASME/ASCE/AHS/ASC
Structures, Structural Dynamics, and Materials Conference, Palm
Springs, CA, April 19-22. |
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Millwater, H.R. et
al. (2004). "Application of Parallel Processing to
Probabilistic Fracture Mechanics Analysis of Gas Turbine
Disks," Proceedings of the 45th
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and
Materials Conference, Palm Springs, CA, April
19-22. |
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Waldhart, C. et al.
(2004). "Methodology for Application of 3-D Stresses to
Surface Damage-Based Risk Assessment,"Proceedings of the 45th AIAA/ASME/ASCE/AHS/ASC
Structures, Structural Dynamics, and Materials Conference, Palm
Springs, CA, April 19-22. |
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Enright, M.P. et
al. (2004). "Probabilistic methodology for life prediction of
aircraft turbine rotors," Proceedings, 9th
Biennial ASCE Aerospace Division International Conference
(Earth and Space), Houston, TX, March 7-10. |
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Leverant, G.R. et
al. (2004). "A new tool for design and certification of aircraft
turbine rotors," Journal of Engineering of
Gas Turbines and Power, Volume 126, pp.
155-159. | |
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| 2003 |
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McClung R.C. et al.
(2003). "The DARWIN® Computer Program for Probabilistic Damage
Tolerance Analysis of Engine Rotors," ADF Aircraft Engine
Symposium, Melbourne, Australia, October 29-30, 2003. |
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Enright, M.P. et
al. (2003). "Probabilistic surface damage tolerance
assessment of aircraft turbine rotors," Proceedings of the 48th ASME International
Gas Turbine & Aeroengine Technical Congress, Atlanta, GA,
June 16-19. |
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Huyse, L. et al.
(2003). "Efficient Statistical Analysis of Failure Risk in
Engine Rotor Disks Using Importance Sampling Techniques," Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC
Structures, Structural Dynamics, and Materials Conference,
Norfolk, VA, April 7-10. |
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Millwater, H.R. et
al. (2003). "Application of an XML-Based Database for
Probabilistic Analysis," Proceedings of
the 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and
Materials Conference, Norfolk, VA, April 7-10. |
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Jameel, A., Lehmann, D., Tschopp, J., and
Dubke, J. (2003). "Application of DARWIN to evaluate risk of
fracture due to material anomalies in gas turbine engines," 6th Annual FAA/Air Force NASA/Navy Workshop on
the Application of Probabilistic Methods to Gas Turbine Engines,
Solomon's Island, MD, March 16-20, 2003. |
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Enright, M.P. et
al. (2003). "Summary of New DARWIN Capabilities for Surface
Damage Tolerance Assessment and Related Enhancements," 6th Annual FAA/Air Force NASA/Navy Workshop on
the Application of Probabilistic Methods to Gas Turbine Engines,
Solomon's Island, MD, March 16-20, 2003. |
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Huyse, L. et al.
(2003). "Recent Probabilistic Computational Efficiency Enhancements
in DARWIN," 6th Annual FAA/Air Force
NASA/Navy Workshop on the Application of Probabilistic Methods to
Gas Turbine Engines, Solomon's Island, MD, March 16-20,
2003. |
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McClung, R.C (2003). "An Executive Update on
the Turbine Rotor Material Design (TRMD) Program," 6th Annual FAA/Air Force NASA/Navy Workshop on
the Application of Probabilistic Methods to Gas Turbine Engines,
Solomon's Island, MD, March 16-20. |
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Laz, P.J. et al.
(2003). "Effect of CTE-induced residual stresses around hard
alpha particles on fatigue crack growth in Ti-6Al-4V," Fatigue and Fracture of Engineering Materials
and Structures Vol. 26, No. 12, pp.
1145-1157. | |
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| 2002 |
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*Leverant, G.R. et
al. (2002). "A new tool for design and certification of aircraft
turbine titanium rotors," Proceedings of the
47th ASME International Gas Turbine & Aeroengine
Technical Congress, Amsterdam, The Netherlands, June
3-6. |
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Wu, Y.-T. et al.
(2002). "Probabilistic Methods for Design Assessment of
Reliability with Inspection," AIAA
Journal, Volume 40, Number 5, pages 937-946. |
|
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Enright, M.P. et
al. (2002). "Optimal sampling techniques for zone-based
probabilistic fatigue life prediction," Proceedings of the 43rd AIAA/ASME/ASCE/AHS/ASC
Structures, Structural Dynamics, and Materials Conference,
Non-Deterministic Approaches Forum, Denver, CO, April 22-25.
|
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Millwater, H.R. et
al. (2002). "A convergent probabilistic technique for risk
assessment of gas turbine disks subject to metallurgical defects,"
Proceedings of the 43rd
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and
Materials Conference, Non-Deterministic Approaches Forum,
Denver, CO, April 22-25. | |
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| 2001 |
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Leverant, G.R. et
al. (2001). "Update on the FAA turbine rotor material design
program," 5th Annual FAA/Air Force/NASA/Navy
Workshop on the Application of Probabilistic Methods for Gas Turbine
Engines, Westlake, Ohio, June 11-13. |
|
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McClung, R.C. et
al. (2001). "Crack nucleation and growth data and modeling," 5th Annual FAA/Air Force/NASA/Navy Workshop on
the Application of Probabilistic Methods for Gas Turbine
Engines, Westlake, Ohio, June 11-13. |
|
|
Millwater, H.R. et
al. (2001). "DARWIN enhancements for probabilistic risk
assessment," 5th Annual FAA/Air
Force/NASA/Navy Workshop on the Application of Probabilistic Methods
for Gas Turbine Engines, Westlake, Ohio, June 11-13.
|
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McClung, R.C. et
al. (2001). "A probabilistic damage tolerance analysis computer
program for engine rotor integrity," AHS
Forum 57, Special Session on Engine Life Management: Addressing
Fleet Risk With Innovative Approaches, Washington, DC, May 9-11.
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| 2000 |
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McKeighan, P.C. et
al. (2000). "Sensing Crack Nucleation and Growth in Hard Alpha
Defects Embedded in Ti-6AI-4V Alloy", Nontraditional Methods of Sensing Stress,
Strain, and Damage in Materials and Structures: Second Volume,
ASTM STP 1323, G.F. Lucas, P.C. McKeighan, and J.S. Ransom,
Eds., American Society for Testing and Materials, West Conshohocken,
PA, 2000. |
|
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Chan, K.S. et al.
(2000). "Constitutive Properties of Hard-Alpha Titanium," Metallurgical and Materials Transactions,
Volume 31A, December 2000. Note: this file is large (11.5 MB)
|
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Wu, Y.-T. (Justin) et
al. (2000). "Efficient and accurate methods for probabilistic
analysis of titanium rotors," Proceedings of
the 8th ASCE Joint Specialty Conference on Probabilistic Mechanics
and Structural Reliability, Notre Dame, IN, July 24-26.
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*Millwater, H.R. et
al. (2000). "A probabilistically-based damage tolerance analysis
computer program for hard alpha anomalies in titanium rotors," Proceedings of the 45th ASME International Gas
Turbine & Aeroengine Technical Congress, Munich, Germany,
May 8-10. |
|
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Wu, Y.-T. (Justin) et
al. (2000). "Probabilistic methods for design assessment of
reliability with inspection (DARWIN)," Proceedings, 41st Structures, Structural
Dynamics, and Materials Conference, Atlanta, GA, April
3-6. |
|
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Enright, M.P. et
al. (2000). "Probabilistic fatigue life sensitivity analysis of
titanium rotors," Proceedings, 41st
Structures, Structural Dynamics, and Materials Conference,
Atlanta, GA, April 3-6. |
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| 1999 |
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McClung, R.C. (1999). "Fracture mechanics
analysis in DARWIN," 4th Annual FAA/USAF
Workshop, Application of Probabilistic Methods to Gas Turbine
Engines, Jacksonville, FL, December 7-8. |
|
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Wu, Y.-T. (Justin), et
al. (1999). "Probabilistic methods for DARWIN," 4th Annual FAA/USAF Workshop, Application of
Probabilistic Methods to Gas Turbine Engines, Jacksonville, FL,
December 7-8. |
|
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Millwater, H.R. et
al. (1999). "A probabilistically-based damage tolerance analysis
computer program for hard alpha defects in titanium rotors," USAF Structural Integrity Program
Conference, San Antonio, TX, Nov. 30. |
|
|
McClung, R.C. et
al. (1999). "Development of a probabilistic design system for
gas turbine rotor inspection," Fatigue '99
The Seventh International Fatigue Conference, Beijing, China,
June 8-12, 2655-2660. |
|
|
McClung, R.C. et
al. (1999). "Fatigue crack growth of titanium rotor alloys in
vacuum and air", Fatigue Behavior of
Titanium Alloys, R. Boyer, D. Eylon, G. Lutjering eds., The
Minerals, Metals & Materials Society, 211-218. |
|
|
McKeighan, P.C. et
al. (1999). "Characterizing the cracking behavior of hard alpha
defects in rotor grade Ti-6-4 Alloy", Fatigue Behavior of Titanium Alloys, R.R.
Boyer, D. Eylon, and G. Lutjering, eds., The Minerals, Metals &
Materials Society.
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| 1997 |
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*Leverant, G.R. et
al. (1997). "A probabilistic approach to aircraft turbine rotor
material design," ASME International Gas
Turbine & Aeroengine Congress ,Paper 97-GT-22. |
|
|
Aerospace Industries Association Rotor
Integrity Sub-Committee(1997). " The development of anomaly
distributions for aircraft engine titanium disk alloys", 38th AIAA/ASME/ASCE/AHS/ASC SDM Conference,
2543-2553. |
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RISC White Paper on AC33.14
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*Copyright ASME. For further information on
ASME publications, visit the ASME web
site. | |
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