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ASTM E2948, Standard Test Method for Conducting Rotating Bending Fatigue Tests of Solid Round Fine Wire, is a procedure for rotating bending fatigue tests of fine wire to obtain the fatigue strength for metallic materials at a specified life in the fatigue regime where the strains are predominately and nominally linear elastic. This method is limited to the fatigue testing of small diameter solid round wire subjected to constant amplitude, completely reversed, periodic strain. The methodology can be useful in assessing the effects of inclusions, melt technique, and cold work processing. Data obtained in accordance with ASTM E2948 is subject to variability because of many factors. An inter-laboratory study (ILS) was performed to assess variability of the data and to develop a precision statement for ASTM E2948. Ten laboratories participated in the ILS. The samples consisted of two materials, Nitinol and 35N LT. Each material was supplied from a single lot from a single manufacturer. Samples were tested at three different strain amplitudes with ten replicates at each strain level. Variability of the resulting data was quantified as reproducibility limits, between laboratory variability, and repeatability limits, within laboratory variability. A precision statement for ASTM E2948 was formulated based on the reproducibility and repeatability limits determined from the inter-laboratory study. The viability of the limits is assessed with Monte Carlo simulations. Alternative methods of analysis using nonparametric statistics and bootstrap methods are discussed.

The use of an analytical model for determining the moduli of elasticity of composite laminates made of woven or unidirectional plies with different porosity levels was described. The analysis of aircraft composite parts with different levels of voids (porosity) was based on a method which utilizes the results of state-of-the-art nondestructive testing methods (ultrasonic through transmission, loading, or pulse/echo) as the starting data for the analytical model. The porosity distribution over the volume of the material and correlations for the nondestructive testing methods were determined for epoxy-carbon laminates with standard and stiffened binders and corroborating experiments were conducted. It was shown that the moduli of elasticity of composite laminates decrease with an increase in the porosity levels. The type, thickness, and layup of the laminate are the basic factors that affect the decrease in the elastic properties of porous composite laminates.

The paper addresses the Plastic behavior of the aluminum alloy 5086 and 5454 in the H-32 temper under cyclic load. It reports the experimental results and analyzes them with the aim to design constitutive laws which could be used in the computational analysis. The reliability of the constitutive laws is analyzed.