| Year |
Citation |
Score |
| 2008 |
van der Walde K, Hillberry BM. Characterization of pitting damage and prediction of remaining fatigue life International Journal of Fatigue. 30: 106-118. DOI: 10.1016/J.Ijfatigue.2007.02.020 |
0.842 |
|
| 2007 |
van der Walde K, Hillberry BM. Initiation and shape development of corrosion-nucleated fatigue cracking International Journal of Fatigue. 29: 1269-1281. DOI: 10.1016/J.Ijfatigue.2006.10.010 |
0.843 |
|
| 2005 |
Maletsky LP, Hillberry BM. Simulating dynamic activities using a five-axis knee simulator. Journal of Biomechanical Engineering. 127: 123-33. PMID 15868795 DOI: 10.1115/1.1846070 |
0.322 |
|
| 2005 |
Van Der Walde K, Brockenbrough JR, Craig BA, Hillberry BM. Multiple fatigue crack growth in pre-corroded 2024-T3 aluminum International Journal of Fatigue. 27: 1509-1518. DOI: 10.1016/J.Ijfatigue.2005.06.026 |
0.835 |
|
| 2004 |
Gruenberg KM, Craig BA, Hillberry BM, Bucci RJ, Hinkle AJ. Predicting fatigue life of pre-corroded 2024-T3 aluminum International Journal of Fatigue. 26: 629-640. DOI: 10.1016/J.Ijfatigue.2003.10.011 |
0.817 |
|
| 2004 |
Gruenberg KM, Craig BA, Hillberry BM, Bucci RJ, Hinkle AJ. Predicting fatigue life of pre-corroded 2024-T3 aluminum from breaking load tests International Journal of Fatigue. 26: 615-627. DOI: 10.1016/J.Ijfatigue.2003.10.010 |
0.8 |
|
| 2004 |
Debartolo EA, Hillberry BM. Predicting fatigue life under spectrum loading in 2024-T3 aluminium using a measured initial flaw size distribution Astm Special Technical Publication. 75-86. |
0.861 |
|
| 2004 |
Sharpe PS, Hillberry BM, Craig BA. Fatigue life variability prediction based on crack forming inclusions in a high strength alloy steel Astm Special Technical Publication. 150-163. |
0.702 |
|
| 2002 |
Moshier MA, Nicholas T, Hillberry BM. High cycle fatigue threshold in the presence of naturally initiated small surface cracks Astm Special Technical Publication. 129-146. |
0.843 |
|
| 2001 |
Laz PJ, Craig BA, Hillberry BM. A probabilistic total fatigue life model incorporating material inhomogeneities, stress level and fracture mechanics International Journal of Fatigue. 23. DOI: 10.1016/S0142-1123(01)00163-3 |
0.687 |
|
| 2001 |
Moshier MA, Nicholas T, Hillberry BM. Load history effects on fatigue crack growth threshold for Ti-6Al-4V and Ti-17 titanium alloys International Journal of Fatigue. 23. DOI: 10.1016/S0142-1123(01)00118-9 |
0.811 |
|
| 2001 |
DeBartolo EA, Hillberry BM. A model of initial flaw sizes in aluminum alloys International Journal of Fatigue. 23. |
0.862 |
|
| 2000 |
Moshier MA, Nicholas T, Hillberry BM. The effect of low cycle fatigue cracks and loading history on high cycle fatigue threshold Astm Special Technical Publication. 427-444. DOI: 10.1520/Stp14813S |
0.851 |
|
| 2000 |
Fragomeni JM, Hillberry BM. Determining the effect of microstructure and heat treatment on the mechanical strengthening behavior of an aluminum alloy containing lithium precipitation hardened with the δ' Al3Li intermetallic phase Journal of Materials Engineering and Performance. 9: 428-440. DOI: 10.1361/105994900770345836 |
0.335 |
|
| 1999 |
Ward GT, Hillberry BM. Approach to include interfacial wear effects in modeling fatigue crack growth of titanium matrix composites Astm Special Technical Publication. 55-75. DOI: 10.1520/Stp13266S |
0.622 |
|
| 1999 |
Moshier MA, Hillberry BM. Inclusion of compressive residual stress effects in crack growth modelling Fatigue and Fracture of Engineering Materials and Structures. 22: 519-526. DOI: 10.1046/j.1460-2695.1999.00182.x |
0.78 |
|
| 1999 |
Zamber JE, Hillberry BM. Probabilistic approach to predicting fatigue lives of corroded 2024-T3 Aiaa Journal. 37: 1311-1317. |
0.675 |
|
| 1998 |
Gruenberg KM, Craig BA, Hillberry BM. Probabilistic method for predicting the variability in fatigue behavior of 7075-T6 aluminum Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 4: 2965-2975. DOI: 10.2514/2.601 |
0.85 |
|
| 1998 |
Laz PJ, Hillberry BM. Fatigue life prediction from inclusion initiated cracks International Journal of Fatigue. 20: 263-270. DOI: 10.1016/S0142-1123(97)00136-9 |
0.725 |
|
| 1998 |
Ward GT, Hillberry BM. An approach to include interfacial wear effects in modeling fatigue crack growth of titanium matrix composites Astm Special Technical Publication. 1330: 55-75. |
0.55 |
|
| 1998 |
DeBartolo EA, Hillberry BM. Effects of constituent particle clusters on fatigue behavior of 2024-T3 aluminum alloy International Journal of Fatigue. 20: 727-735. |
0.828 |
|
| 1998 |
Gruenberg KM, Craig BA, Hillberry BM. Probabilistic method for predicting the variability in fatigue behavior of 7075-T6 aluminum Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 4: 2965-2975. |
0.85 |
|
| 1997 |
Herrmann DJ, Hillberry BM. Effects of fiber bridging and fiber fracture on fatigue cracking in a titanium-matrix composite Astm Special Technical Publication. 1285: 103-125. DOI: 10.1520/Stp19924S |
0.639 |
|
| 1997 |
Herrmann DJ, Hillberry BM. A new approach to the analysis of unidirectional titanium matrix composites with bridge and unbridged cracks Engineering Fracture Mechanics. 56: 711-726. |
0.403 |
|
| 1996 |
Herrmann DJ, Ward GT, Lawson EJ, Hillberry BM. Prediction of matrix fatigue crack initiation from notches in titanium matrix composites Astm Special Technical Publication. 1253: 359-376. DOI: 10.1520/Stp18231S |
0.625 |
|
| 1995 |
Johnson W, Masters J, Ward G, Herrmann D, Hillberry B. Fatigue-Life Behavior and Matrix Fatigue Crack Spacing in Unnotched SCS-6/Timetal®21S Metal Matrix Composites Journal of Composites Technology and Research. 17: 205. DOI: 10.1520/CTR10484J |
0.518 |
|
| 1995 |
Laz PJ, Hillberry BM. Probabilistic approach to the generation of EIFS distributions derived from inclusion characteristics American Society of Mechanical Engineers, Aerospace Division (Publication) Ad. 47: 81-85. |
0.487 |
|
| 1993 |
Hillberry BM, Johnson WS. Fatigue crack spacing in the matrix of a continuous fiber SCS-6/Ti composite Journal of Composites Technology and Research. 15: 210-216. |
0.607 |
|
| 1992 |
Johnson W, Masters J, Kevin O'Brien T, Hillberry B, Steven Johnson W. Prediction of Matrix Fatigue Crack Initiation in Notched SCS-6/Ti-15-3 Metal Matrix Composites Journal of Composites Technology and Research. 14: 221. DOI: 10.1520/CTR10101J |
0.491 |
|
| 1992 |
Dougherty DJ, de Koning AU, Hillberry BM. Modeling high crack growth rates under variable amplitude loading Astm Special Technical Publication. 214-233. |
0.636 |
|
| 1990 |
Hillberry BM, Johnson WS. Matrix fatigue crack development in a notched continuous fiber SCS-6/Ti-15-3 composite American Society of Mechanical Engineers, Applied Mechanics Division, Amd. 111: 121-127. |
0.625 |
|
| 1983 |
Ostergaard DF, Hillberry BM. CHARACTERIZATION OF THE VARIABILITY IN FATIGUE CRACK PROPAGATION DATA Astm Special Technical Publication. 97-115. |
0.612 |
|
| 1979 |
Virkler DA, Hillberry BM, Goel PK. STATISTICAL NATURE OF FATIGUE CRACK PROPAGATION Journal of Engineering Materials and Technology, Transactions of the Asme. 101: 148-153. |
0.575 |
|
| 1978 |
Rueping JE, Hillberry BM, Mettler SC, Stevenson WH. COMPARATIVE STUDY OF FATIGUE CRACK CLOSURE Aiaa Journal. 16: 413-415. |
0.619 |
|
| 1976 |
Himmelein M, Hillberry B. Effect of stress ratio and overload ratio on fatigue crack delay and arrest behavior due to single peak overloads Astm Special Technical Publications. 321-330. DOI: 10.1520/Stp33954S |
0.514 |
|
| 1975 |
Hillberry BM, Alzos WX, Skat AC. FATIGUE CRACK PROPAGATION DELAY BEHAVIOR IN 2024-T3 ALUMINUM ALLOY DUE TO SINGLE OVERLOAD/UNDERLOAD SEQUENCES Us Air Force Syst Command Air Force Flight Dyn Lab Tech Rep Affdl-Tr-75-96. |
0.616 |
|
| 1974 |
Probst EP, Hillberry BM. FATIGUE CRACK DELAY AND ARREST DUE TO SINGLE PEAK TENSILE OVERLOADS Aiaa Journal. 12: 330-335. |
0.666 |
|
| 1972 |
HILLBERRY BM, HAMILTON JF. IMPROVEMENT IN FATIGUE BEHAVIOUR BY OVERLOADING . JULY 25-27, 1972. |
0.495 |
|
| 1971 |
Kessler AF, Hillberry BM. The effect of periodic overstress on the fatigue life of notched aluminum specimens Sae Technical Papers. DOI: 10.4271/710599 |
0.556 |
|
| 1971 |
Linsley RC, Hillberry BM. RANDOM FATIGUE OF 2024-T3 ALUMINUM UNDER TWO SPECTRA WITH IDENTICAL PEAK-PROBABILITY DENSITY FUNCTIONS Astm Special Technical Publication. 156-167. |
0.366 |
|
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