Due to their excellent strength-to-weight and stiffness-to-weight ratios, thin sheets of composite materials are increasingly being used for lightweight applications such as in the transportation industry or for high end sports equipment. [1][2][3][4] To optimize the weight of a structure by pushing its loading as close as reasonably possible to the load-carrying capacity of the material, accurate design guidelines are needed that take the anisotropy of the material into account. For notched composite structures where the load carrying capacity is limited by fracture from the notch-rather than delamination-this means that accurate and usable solutions are required to determine the stress concentration factor K t at the notch tip or, in the presence of a crack emanating from the notch tip, the stress intensity factor K 1 .Over the past decades, stress concentration factors have been determined for a wide variety of notched geometries. Among the most comprehensive and authoritative compilations is the one by Peterson. [5,6] For anisotropic materials, however, K t and K 1 solutions are hard to find. Very few solutions have been published for stress concentration factors in anisotropic materials, [7][8][9][10][11][12] and even less so for stress intensity factors of cracks emanating from notches. [13] The present study addresses this problem. It focuses on the strength calculation of notched composite structures where the load carrying capacity is limited by fracture of through the thickness cracks emanating from the notch. Two design guidelines the applicabilities of which are well proven for isotropic materials-the stress concentration factor concept and the weight function technique-will be extended to equibiaxial orthotropic materials, i.e., orthotropic materials with equal mechanical properties in both principal directions. With the results of this study, it is possible to predict the strength of notched structures made of these materials more accurately.
Anisotropic ElasticityWithin linear elasticity, the stress-strain relation in an anisotropic material is described bywhere e i , S ij , and s j are the strain tensor, the compliance matrix, and the stress tensor, respectively. In a cubic material, S ij consists of the three independent components S 11 , S 12 , and S 66 . Alternatively, engineering quantities, e.g., direction dependent Young's moduli and Poisson's ratios, can be used, see e.g., Kalamkarov. [14] In this study, E 1 , n 12 , and E 458 are employed, where the subscripts 1 and 12 refer to the principal axes of the material, and the subscript 458 to a direction rotated by 458. Using engineering properties is convenient because Poisson's ratio n 12 shows to be of negligible influence on the calculated K t and K 1 values. This reduces the number ofIn notched structures, the influence of the notch on the structural strength of the component can be described by a stress concentration factor or-in the presence of cracks-a weight function. Numerous stress concentration factor and weight function solutions a...