selected publications
-
academic article
- Results of a Pilot Study in Support of a Round-Robin on Creep-Fatigue Crack Growth Testing of a Creep-Brittle Material for ASTM E2760. Materials Performance and Characterization. 11. 2022
- Creep behavior of Alloy 709 at 700 degrees C. Materials Science and Engineering A - Structural Materials Properties Microstructure and Processing. 762:138083. 2019
- The influence of plasticity-induced crack closure on creep-fatigue crack growth in two heat-resistant steels. International Journal of Fatigue. 125:291-298. 2019
- Relative stiffness of 3 bandage/splint constructs for stabilization of equine midmetacarpal fractures. Journal of Veterinary Emergency and Critical Care. 25:379-387. 2015
- Thermal Stresses Due to Laser Welding in Bridge-Wire Initiators. Journal of Electronic Packaging. 131. 2009
- Thermal Induced Stresses in Bridge-Wire Initiator Glass-to-Metal Seals. Journal of Electronic Packaging. 129:300-306. 2006
- Fatigue crack growth and life predictions under variable amplitude loading for a cast and wrought aluminum alloy. International Journal of Fatigue. 28:53-60. 2006
- Fatigue crack growth in two advanced titanium alloys under constant and variable amplitude loading at 25 and 175 degrees C. Fatigue and Fracture of Engineering Materials and Structures. 21:819-834. 2002
- Fatigue crack growth of Ti-62222 titanium alloy under constant amplitude and miniTWIST flight spectra at 25 degrees C and 175 degrees C. International Journal of Fatigue. 19:301-308. 1997
- Fatigue crack growth of beta-21S titanium alloy under constant amplitude and miniTWIST flight spectra at 25 degrees C and 175 degrees C. Journal of Engineering Materials and Technology-transactions of the Asme. 119:387-392. 1997
-
conference paper
- Volumetric and surface positron annihilation studies of fatigue damage accumulation in a steel alloy. Fatigue and Fracture Mechanics: 35th Volume. 158-167. 2007
- Effect of transient loads on fatigue crack growth in solution treated and aged Ti-62222 at -54, 25, and 175 degrees C. Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions. 154-170. 2005
- Effect of geometry and load history on fatigue-crack growth in Ti-62222. Fatigue Crack Growth Thresholds, Endurance Limits, and Design. 175-191. 2000
- Role of crack closure mechanisms on fatigue crack growth of Ti-62222 under constant-amplitude and transient loading at-54, 25, and 175 degrees C. Advances in Fatigue Crack Closure Measurement and Analysis: Second Volume. 224-245. 1999
- Comparison of constant and variable amplitude loading on FCG of two advanced titanium alloys at 25 degrees C and 175 degrees C. Icaf 97: Fatigue in New and Ageing Aircraft, Vols I and Ii: Vol I: Lecture Papers, Vol Ii: Poster Papers. 779-790. 1997