Slice synthesis method, which was fu'st proposed by Bluhm [1], has been found to be an efficient approximate analytical method in deriving compliance for fracture specimens with complex crack or circumference configurations. Compliance data are important for fracture analysis and testing. Compliance of three-point bend (3PB) round bars, derived by using slice synthesis method, has been given for those with straight-through cracks [2,3] and with chevron-notch cracks [3,4]. Round bars of brittle material could be tested more stably than their square counterpart, however, in some situations, modified round bars (with parallel flattened planes) are more appropriate in specimen preparation and testing [5]. In this report we present wide range compliance of flattened three-point bend round bars (Fig. 1), which is an extension of our previous work [2][3][4]. If flattened height W 0 is equal to D (the diameter), the case of the original unflattened height, solved in [2-4], is restored. The basic formulation or trace of the formulation can be found in [2-4], and will not be repeated here, only those formulations related to the new feature of the flattened part will be given below.In Fig. 1, a is the nominal crack length, a' is the actual crack length, which is not shown in Fig. 1, and D-W0For convenient presenting of the derived results, only a is used in the formulation and Tables of the compliance data, although a' is more direct in practical use, however, a' is easily correlated with a through (1). B 0 is the thickness of the flattened plane, the relation between B 0, W 0 and D is as follows:W0/D determines the configuration of the flattened part hence it is given in the Tables as a variable.