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In order to evaluate their applicability as a design formula for SCC specimens, experimental results obtained from this study were compared with the prediction results by the aforementioned methods.
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This paper presents primarily the design of the specimen, experimental results, and simplified analytical modeling techniques for Phase I specimen.
Comparison of calculated force displacement relationship of the studied column specimens against experimental results are illustrated in Fig. 9f i for A2, A4, A8 and A10 column specimens, respectively.
Open image in new window Fig. 7 Validation of FE dog-bone specimens with experimental results: a brick plain concrete and b brick SFRC with enlarged end fibers Open image in new window Fig. 8 Validation of FE dog-bone specimens with experimental results: a stone plain concrete and b stone SFRC with enlarged end fibers Open image in new window Fig. 9 Deformed shapes.
Following a short description of the specific device designed to produce a thermal gradient in the thickness of wall specimens, the experimental results are presented together with the corresponding calculations.
Specimen-level experimental results were analyzed using criteria similar to those adopted in Yamamoto et al. (2003), which are summarized in the upper column of Table 1.
Specimen-level experimental results were analyzed on Arai plots (Arai 1963; Nagata et al. 1963) using the Thellier GUI program included in the "PmagPy" software package by Shaar and Tauxe (2013), based on criteria summarized in the upper column of Table 2, which were similar to those adopted in Cromwell et al. (2015).
Size effect of the test specimens on the experimental results is well analyzed by the proposed method.
A close agreement between the numerically predicted deflected shapes of the specimen and the experimental results indicated that the stress strain distributions from the numerical elastic plastic model could be applied with reasonable accuracy.
The low velocity impact tests were also simulated with the help of finite element analysis (FEA) techniques of ABAQUS® software in order to predict and compare the crashworthiness of each category of specimen model with experimental results.
The predicted fatigue life and crack initiation position for CT scanned specimens were compared with experimental results.
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