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1
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84865459129
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Aircraft accident report - United Airlines Flight 232 McDonnell Douglas DC-10-10 Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
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Washington, DC.
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1National Transportation Safety Board, "Aircraft Accident Report - United Airlines Flight 232 McDonnell Douglas DC-10-10 Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989", NTSB/AAR-90/06, Washington, DC., 1990.
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NTSB/AAR-90/06
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2
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84903774149
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Advisory circular - Damage tolerance for high energy turbine engine rotors
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U.S. Department of Transportation, Washington, DC
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2Federal Aviation Administration, "Advisory Circular - Damage Tolerance for High Energy Turbine Engine Rotors," AC 33.14-1, U.S. Department of Transportation, Washington, DC., 2001.
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(2001)
AC 33.14-1
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3
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13644253082
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A new tool for design and certification of aircraft turbine rotors
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ASME
-
Leverant, G.R., McClung, R.C., Millwater, H.R., and Enright, M.P. , "A New Tool for Design and Certification of Aircraft Turbine Rotors", Journal of Engineering for Gas Turbines and Power, ASME,Vol. 126, No. 1, 2003, pp. 155-159.
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(2003)
Journal of Engineering for Gas Turbines and Power
, vol.126
, Issue.1
, pp. 155-159
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Leverant, G.R.1
McClung, R.C.2
Millwater, H.R.3
Enright, M.P.4
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4
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27744604330
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A software framework for probabilistic fatigue life assessment
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Paper ID JAII1563
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McClung, R.C., Enright, M.P., Millwater, H.R., Leverent, G.R., and Hudak, S.J., "A Software Framework for Probabilistic Fatigue Life Assessment," Journal of ASTM International, Vol. 1, No. 8, 2004, Paper ID JAII1563.
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Journal of ASTM International
, vol.1
, Issue.8
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McClung, R.C.1
Enright, M.P.2
Millwater, H.R.3
Leverent, G.R.4
Hudak, S.J.5
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6
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-
0036572671
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Probabilistic methods for design assessment of reliability with inspection
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Wu, Y.T., Enright, M.P., and Millwater, H.R., "Probabilistic Methods for Design Assessment of Reliability with Inspection," AIAA Journal, Vol. 40, No. 5, 2002, pp. 937-946.
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(2002)
AIAA Journal
, vol.40
, Issue.5
, pp. 937-946
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Wu, Y.T.1
Enright, M.P.2
Millwater, H.R.3
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7
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0013276157
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Turbine rotor material design - Final report
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Federal Aviation Administration, Washington, DC
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Leverant, G.R., "Turbine Rotor Material Design - Final Report," DOT/ FAA/ AR-00/64, Federal Aviation Administration, Washington, DC, 2000.
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DOT/ FAA/ AR-00/64
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Leverant, G.R.1
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8
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84888800691
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Efficient fracture design for complex turbine engine components
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ASME, (accepted)
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McClung, R.C., Enright, M.P., Lee, Y-D., Huyse, L., and Fitch, S.H.K, "Efficient Fracture Design for Complex Turbine Engine Components," Journal of Engineering for Gas Turbines and Power, ASME, 2005, (accepted).
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(2005)
Journal of Engineering for Gas Turbines and Power
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McClung, R.C.1
Enright, M.P.2
Lee, Y.-D.3
Huyse, L.4
Fitch, S.H.K.5
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9
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0003427095
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John Wiley, New York
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Haldar, A. and Mahadevan, S., Probability, Reliability, and Statistical Methods in Engineering Design, John Wiley, New York, 2000.
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Probability, Reliability, and Statistical Methods in Engineering Design
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Haldar, A.1
Mahadevan, S.2
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10
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0000272735
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The analysis of structural safety
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ASCE
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Freudenthal, A.M., Garrelts, J.M, and Shinozuka, M., "The Analysis of Structural Safety." Journal of the Structural Division, ASCE, Vol. 92, No. ST1, 1966, pp. 267-325.
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Freudenthal, A.M.1
Garrelts, J.M.2
Shinozuka, M.3
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11
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0030645507
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The development of anomaly distributions for aircraft engine titanium disk alloys
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Kissimmee, FL, April 7-10
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10Aerospace Industries Association Rotor Integrity Subcommittee. "The Development of Anomaly Distributions for Aircraft Engine Titanium Disk Alloys," Proceedings 38th Structures, Structural Dynamics, and Materials Conference, Kissimmee, FL, April 7-10, 1997, pp. 2543-2553.
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Proceedings 38th Structures, Structural Dynamics, and Materials Conference
, pp. 2543-2553
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12
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-
34848815898
-
A convergent zone-refinement method for risk assessment of gas turbine disks subject to low-frequency metallurgical defects
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ASME. (submitted)
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Millwater, H.R., Enright, M.P., and Fitch, S.H.K., "A Convergent Zone-Refinement Method for Risk Assessment of Gas Turbine Disks Subject to Low-Frequency Metallurgical Defects," Journal of Engineering for Gas Turbines and Power, ASME. (submitted).
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Journal of Engineering for Gas Turbines and Power
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Millwater, H.R.1
Enright, M.P.2
Fitch, S.H.K.3
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13
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0031148367
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Fatigue failure probability in a powder metallurgy Ni-base superalloy
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Grison. J. and Remy, L. "Fatigue Failure Probability in a Powder Metallurgy Ni-Base Superalloy,'' Engineering Fracture Mechanics, Vol. 57, No. 1, 1997, pp. 41-55.
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Engineering Fracture Mechanics
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, Issue.1
, pp. 41-55
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Grison, J.1
Remy, L.2
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14
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0034773172
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Stages of fatigue fracture in nickel alloyed powder metallurgy steel
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Drar, H., "Stages of Fatigue Fracture in Nickel Alloyed Powder Metallurgy Steel." Materials Science and Technology, Vol. 17, 2001, pp. 1259-1264.
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Materials Science and Technology
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Drar, H.1
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15
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28844439972
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Probabilistic rotor design system - Final report
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Air Force Research Laboratory, Cincinnati, OH
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Roth, P.G., "Probabilistic Rotor Design System - Final Report", AFRL-PR-WP-TR-1999-2122, Air Force Research Laboratory, Cincinnati, OH, 1998.
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(1998)
AFRL-PR-WP-TR-1999-2122
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Roth, P.G.1
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16
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-
0032660969
-
Probabilistic analysis of aircraft gas turbine disk life and reliability
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ASME
-
Melis, M.E. and Zaretsky, E.V., "Probabilistic Analysis of Aircraft Gas Turbine Disk Life and Reliability," Journal of Propulsion and Power, ASME, Vol. 15, No. 5, 1999, pp. 658-666.
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(1999)
Journal of Propulsion and Power
, vol.15
, Issue.5
, pp. 658-666
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Melis, M.E.1
Zaretsky, E.V.2
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17
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-
0035480269
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Fracture analysis of turbine disks and computational-experimental background of the operational decisions
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Shlyannikov, V.N., Iltchenko, B.V., and Stepanov, N.V., "Fracture Analysis of Turbine Disks and Computational-Experimental Background of the Operational Decisions," Engineering Failure Analysis, Vol. 8. 2001, pp. 461-475.
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Engineering Failure Analysis
, vol.8
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Shlyannikov, V.N.1
Iltchenko, B.V.2
Stepanov, N.V.3
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18
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28844442694
-
Aircraft accident report - Uncontained engine failure, Delta Air Lines Flight 1288, McDonnell Douglas MD-88, N927DA
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Washington, DC
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17National Transportation Safety Board "Aircraft Accident Report - Uncontained Engine Failure, Delta Air Lines Flight 1288, McDonnell Douglas MD-88, N927DA," NTSB/AAR-98/01, Washington, DC, 1996.
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(1996)
NTSB/AAR-98/01
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19
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27744433159
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A probabilistic framework for risk prediction of engine components with inherent and induced material anomalies
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accepted
-
Enright, M.P., McClung, R.C., and Huyse, L., "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, 2005 (accepted).
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(2005)
Proceedings 50th ASME International Gas Turbine & Aeroengine Technical Congress, Reno, NV, June 6-9
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-
Enright, M.P.1
McClung, R.C.2
Huyse, L.3
-
20
-
-
0043011599
-
Efficient statistical analysis of failure risk in engine rotor disks using importance sampling techniques
-
Norfolk, VA, April 7-10, AIAA Paper 2003-1838
-
Huyse, L., and Enright, M.P., "Efficient Statistical Analysis of Failure Risk in Engine Rotor Disks using Importance Sampling Techniques," Proceedings 44th Structures, Structural Dynamics, and Materials Conference, Norfolk, VA, April 7-10, 2003, AIAA Paper 2003-1838.
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Proceedings 44th Structures, Structural Dynamics, and Materials Conference
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-
Huyse, L.1
Enright, M.P.2
-
21
-
-
27744510251
-
Fracture mechanics-based probabilistic life prediction of components with large numbers of inherent material anomalies
-
Rome, Italy, June 19-22, (accepted)
-
Enright, M.P., McClung, R.C., and Huyse, L., "Fracture Mechanics-Based Probabilistic Life Prediction of Components With Large Numbers of Inherent Material Anomalies", Ninth International Conference on Structural Safety and Reliability (ICOSSAR), Rome, Italy, June 19-22, 2005 (accepted).
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(2005)
Ninth International Conference on Structural Safety and Reliability (ICOSSAR)
-
-
Enright, M.P.1
McClung, R.C.2
Huyse, L.3
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