Detailed Record



An Expanded Wing Crack Model for Fracture and Mechanical Behavior of Sandstone Under Triaxial Compression


Abstract A new model is developed to predict the mechanical behavior of brittle sandstone under triaxial compression. The proposed model aims to determine the normalized critical crack length (Lcr), through which the failure strength (σf) of sandstone can be estimated based on fracture mechanics applied to secondary cracks emanating from pre-existing flaws, while considering the interaction of neighboring cracks. In this study, the wing crack model developed by Ashby and Hallam (1986) was adopted to account for the total stress intensity at the crack tip (KI) as the summation of the stress intensity due to crack initiation and crack interaction. The proposed model is developed by first deriving the Lcr and then setting the crack length equal to the Lcr. Next, the total stress intensity is set equal to the rock fracture toughness in the original equation of KI, resulting in an estimate of the σf. Finally, to evaluate the performance of the proposed model on predicting σf, theoretical results are compared with laboratory data obtained on sandstone formations collected from Wyoming and the published literature. Moreover, the σf predicted by our proposed model is compared with those predicted from other failure criteria from the literature. The comparison shows that the proposed model better predicts the rock failure strength under triaxial compression, based on the lowest RMSE and MAD values of 36.95 and 30.93, respectively.
Authors Esraa Saleh Alomari University of WyomingORCID , Kam Ng University of WyomingORCID , Lokendra Khatri University of WyomingORCID
Journal Info Multidisciplinary Digital Publishing Institute | Materials , vol: 17 , iss: 23 , pages: 5973 - 5973
Publication Date 12/6/2024
ISSN 1996-1944
TypeKeyword Image article
Open Access gold Gold Access
DOI https://doi.org/10.3390/ma17235973
KeywordsKeyword Image