Cite
Theoretical-Experimental Model for Predicting Crack Growth Rate in Structural Alloys of Aircraft Gas Turbine Engine Disks with Regard to Fatigue and Creep.
MLA
Pokrovskii, V., et al. “Theoretical-Experimental Model for Predicting Crack Growth Rate in Structural Alloys of Aircraft Gas Turbine Engine Disks with Regard to Fatigue and Creep.” Strength of Materials, vol. 37, no. 6, Nov. 2005, pp. 558–65. EBSCOhost, https://doi.org/10.1007/s11223-006-0002-0.
APA
Pokrovskii, V., Ezhov, V., & Sidyachenko, V. (2005). Theoretical-Experimental Model for Predicting Crack Growth Rate in Structural Alloys of Aircraft Gas Turbine Engine Disks with Regard to Fatigue and Creep. Strength of Materials, 37(6), 558–565. https://doi.org/10.1007/s11223-006-0002-0
Chicago
Pokrovskii, V., V. Ezhov, and V. Sidyachenko. 2005. “Theoretical-Experimental Model for Predicting Crack Growth Rate in Structural Alloys of Aircraft Gas Turbine Engine Disks with Regard to Fatigue and Creep.” Strength of Materials 37 (6): 558–65. doi:10.1007/s11223-006-0002-0.