-
1
-
-
6944245663
-
Engine component retirement for cause
-
AFWAL-TR-87-4069
-
Harris, J. A., Jr., "Engine Component Retirement for Cause," AFWAL-TR-87-4069, Volume I - Executive Summary, 1987.
-
(1987)
Volume I - Executive Summary
, vol.1
-
-
Harris Jr., J.A.1
-
2
-
-
6944242094
-
Probabilistic Rotor Design System (PRDS) phase I
-
WL-TR-92-2011
-
Roth, P. G., "Probabilistic Rotor Design System (PRDS) Phase I," GE Aircraft Engines, WL-TR-92-2011, 1992.
-
(1992)
GE Aircraft Engines
-
-
Roth, P.G.1
-
3
-
-
33646092078
-
Probabilistic design system - Phase I and II interim report
-
Adamson, J. D., Fox, E. P., and Malone, J. E., "Probabilistic Design System - Phase I and II Interim Report," Pratt & Whitney Report FR-24004-1, 1995.
-
(1995)
Pratt & Whitney Report
, vol.FR-24004-1
-
-
Adamson, J.D.1
Fox, E.P.2
Malone, J.E.3
-
4
-
-
0013276157
-
Turbine rotor material design
-
DOT/FAA/AR-00/64
-
Leverant, G. R., et al., "Turbine Rotor Material Design," Final Report, DOT/FAA/AR-00/64, 2000.
-
(2000)
Final Report
-
-
Leverant, G.R.1
-
5
-
-
0346965634
-
Probabilistic surface damage tolerance assessment of aircraft turbine rotors
-
Atlanta, Georgia
-
Enright, M. P., Lee, Y.-D., McClung, R. C., Huyse, L., Leverant, G. R., Millwater, H. R., et al., "Probabilistic Surface Damage Tolerance Assessment Of Aircraft Turbine Rotors," 48th ASME International Gas Turbine & Aeroengine Technical Congress, Atlanta, Georgia, 2003.
-
(2003)
48th ASME International Gas Turbine & Aeroengine Technical Congress
-
-
Enright, M.P.1
Lee, Y.-D.2
McClung, R.C.3
Huyse, L.4
Leverant, G.R.5
Millwater, H.R.6
-
6
-
-
33244464803
-
Enhanced prognosis through probabilistic damage assessment
-
Wright Laboratory, Air Force Material Command, June
-
Hudak, S. J., Jr., Enright, M. P., McClung, R. C., Millwater, H. R., Sarlashkar, A., and Roemer, M. J., "Enhanced Prognosis Through Probabilistic Damage Assessment," Final Report to Materials Directorate, Wright Laboratory, Air Force Material Command, June 2002.
-
(2002)
Final Report to Materials Directorate
-
-
Hudak Jr., S.J.1
Enright, M.P.2
McClung, R.C.3
Millwater, H.R.4
Sarlashkar, A.5
Roemer, M.J.6
-
7
-
-
80051808528
-
A convergent probabilistic technique for risk assessment of gas turbine disks subject to metallurgical defects
-
AIAA 2002-1382, Denver, CO
-
Millwater, H. R., Enright, M. P., and Fitch, S. H. K., "A Convergent Probabilistic Technique for Risk Assessment of Gas Turbine Disks Subject to Metallurgical Defects," AIAA 2002-1382, 43rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Denver, CO, 2002.
-
(2002)
43rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
-
-
Millwater, H.R.1
Enright, M.P.2
Fitch, S.H.K.3
-
8
-
-
0036572671
-
Probabilistic methods for design assessment of reliability with inspection
-
Wu, Y.-T., Enright, M. P., and Millwater, H. R., "Probabilistic Methods for Design Assessment of Reliability with Inspection," AIAA Journal, Vol. 40, 2002, pp. 937-946.
-
(2002)
AIAA Journal
, vol.40
, pp. 937-946
-
-
Wu, Y.-T.1
Enright, M.P.2
Millwater, H.R.3
-
9
-
-
84896693535
-
Efficient statistical analysis of failure risk in engine rotor disks using importance sampling techniques
-
AIAA 2003-1838, Norfolk, Virginia
-
Huyse, L., and Enright, M. P., "Efficient Statistical Analysis of Failure Risk in Engine Rotor Disks Using Importance Sampling Techniques," AIAA 2003-1838, 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Norfolk, Virginia, 2003.
-
(2003)
44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
-
-
Huyse, L.1
Enright, M.P.2
-
10
-
-
6944239407
-
-
Advisory Circular 33.14-1, Federal Aviation Administration, January 8
-
"Damage Tolerance for High Energy Turbine Engine Rotors," Advisory Circular 33.14-1, Federal Aviation Administration, January 8, 2001.
-
(2001)
Damage Tolerance for High Energy Turbine Engine Rotors
-
-
-
12
-
-
84920632474
-
AGARD engine disc cooperative test programme
-
Morn, A. J. A., and Raizenne, M. D., "AGARD Engine Disc Cooperative Test Programme," AGARD Report 766, 1988.
-
(1988)
AGARD Report
, vol.766
-
-
Morn, A.J.A.1
Raizenne, M.D.2
-
13
-
-
6944249763
-
-
Laboratory Memorandum ST-479, National Aeronautical Establishment, Ottawa, Canada
-
Raizenne, M. D., "Fatigue Crack Growth Rate Data for AGARD TX114 Engine Disc Cooperative Test Programme," Laboratory Memorandum ST-479, National Aeronautical Establishment, Ottawa, Canada, 1987.
-
(1987)
Fatigue Crack Growth Rate Data for AGARD TX114 Engine Disc Cooperative Test Programme
-
-
Raizenne, M.D.1
-
14
-
-
0012034228
-
Fatigue crack initiation modeling in Ti-6A1-4V for smooth and notched geometries
-
Chandler, AZ
-
Slavik, D. C., Dunyak, T., Griffiths, J., and Kurath, P., "Fatigue Crack Initiation Modeling in Ti-6A1-4V for Smooth and Notched Geometries," Proceedings of the 5th National Turbine Engine High Cycle Fatigue Conference, Chandler, AZ, 2000.
-
(2000)
Proceedings of the 5th National Turbine Engine High Cycle Fatigue Conference
-
-
Slavik, D.C.1
Dunyak, T.2
Griffiths, J.3
Kurath, P.4
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