TY - GEN
T1 - Prediction of maximum crack length in longitudinal varestraint testing
AU - Robino, C. V.
AU - Reece, M.
AU - Knorovsky, G. A.
AU - DuPont, J. N.
AU - Feng, Z.
PY - 2005
Y1 - 2005
N2 - High speed, high resolution video observations of solidification cracking in longitudinal Varestraint tests of Alloy 718 reveal a number of important features of the test. For large augmented strains, crack initiation occurs at a liquid fraction of approximately 0.2, and crack growth proceeds in both advancing (growth in the torch travel direction) and retreating (growth away from the trailing edge) directions. For the advancing crack, the average growth velocity is identical to the travel speed, indicating that the advancing tip grows at isothermal temperature and consequently, a fixed liquid fraction. Termination of the advancing crack tip occurs as the augmented strain field diminishes. The retreating crack tip grows in an increasing strain field and decreasing temperature, and appears to terminate when the crack tip intersects the solidus. These observations define criteria for the major events governing the maximum crack length at high augmented strains. Coupling these criteria with models of strain development, temperature distribution, and solidification behavior allows for a priori estimation of the maximum crack length. In the present work, the maximum crack length for a variety of Nb-containing Fe and Ni-based superalloys are estimated by using the above models and criteria, and compared with experimental results.
AB - High speed, high resolution video observations of solidification cracking in longitudinal Varestraint tests of Alloy 718 reveal a number of important features of the test. For large augmented strains, crack initiation occurs at a liquid fraction of approximately 0.2, and crack growth proceeds in both advancing (growth in the torch travel direction) and retreating (growth away from the trailing edge) directions. For the advancing crack, the average growth velocity is identical to the travel speed, indicating that the advancing tip grows at isothermal temperature and consequently, a fixed liquid fraction. Termination of the advancing crack tip occurs as the augmented strain field diminishes. The retreating crack tip grows in an increasing strain field and decreasing temperature, and appears to terminate when the crack tip intersects the solidus. These observations define criteria for the major events governing the maximum crack length at high augmented strains. Coupling these criteria with models of strain development, temperature distribution, and solidification behavior allows for a priori estimation of the maximum crack length. In the present work, the maximum crack length for a variety of Nb-containing Fe and Ni-based superalloys are estimated by using the above models and criteria, and compared with experimental results.
UR - http://www.scopus.com/inward/record.url?scp=33751518144&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:33751518144
SN - 0871708426
SN - 9780871708427
T3 - ASM Proceedings of the International Conference: Trends in Welding Research
SP - 313
EP - 318
BT - Trends in Welding Research - Proceedings of the 7th International Conference
T2 - 7th International Conference on Trends in Welding Research
Y2 - 16 May 2005 through 20 May 2005
ER -