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Herein, lattice‐specific elastic stiffnesses of a structural alloy with commercial, medical, and military aircraft applications are investigated by neutron diffraction. Macroscopic mechanical properties are characterized by conventional techniques and response to thermally induced strains is probed by X‐ray diffraction (XRD); these findings are compared to data given by neutron diffraction tools. The material used in this study is the forged Ti64 titanium alloy (6% aluminum and 4% vanadium). Diffraction elastic constants are found to range from 114 GPa to 138 GPa. Macroscopic moduli of 118 GPa and 116 GPa are found from extensometry and digital imaging correlation, respectively. The (101) reflection is the reflection that best matches the macroscopic material behavior with a modulus of 117 GPa for the studied material. The effect of mechanical and thermal strains on the axial ratio of the crystal structure is investigated. Texture is an important consideration when comparing micro‐ and macro‐scale behavior; texture from electron backscatter diffraction (EBSD) maps reveals minimal preferred orientation for the material under study thus indicating (101) planes suitably reflect overall material behavior. [ABSTRACT FROM AUTHOR]

Carbon fiber-reinforced vinyl ester composite facings are being considered by the US Navy for sandwich structures with either low-density polyvinyl chloride foam or balsa wood as the core materials manufactured using Vacuum-Assisted Resin Transfer Molding process. In this paper, experimental techniques are developed to evaluate the variation of surface strain spatially using three-dimensional Digital Image Correlation technique and internal damage evolution using radiation-based tomography. Both X-ray and neutron radiation was utilized to evaluate the microstructure of composite laminate facings in three dimensions at high resolution. Since naval structures are exposed to harsh sea environment, samples were soaked in simulated sea water at 40℃ for long duration, well beyond saturation stage of Fickian diffusion ascertained using weight gain measurements. Results for a series of mechanical tests on fiber dominated samples of [0/90]2S and matrix dominated samples of [±45]2S orientation are reported. Variable specimen sizes (12.5 mm wide by 100 mm long, 25 mm by 200 mm, and 25 mm by 300 mm, all with an average uniform thickness of 2.8 mm) for laboratory tests are utilized in order to evaluate the applicability of results for large ship structures. Different carbon fiber-reinforced vinyl ester failure mechanisms of matrix crack interactions, such as matrix dominated transverse tension, tension along fibers, and fiber delamination were observed. Digital Image Correlation technique was useful to track the existence of localized damage for both fiber and matrix dominated carbon fiber-reinforced vinyl ester laminates. High resolution X-ray and neutron tomography under in-situ mechanical loading were used to investigate interior microstructure evolution and damage at chosen stress levels. The new techniques presented in this paper can enable a comparison between interior specimen damage and surface damage (readily observable using Digital Image Correlation). Use of different modality of radiation (neutrons versus X-rays) was very useful to probe damage resulting from moisture diffused in the matrix resin and fiber interface/interphase and shows a lot of promise for studying the failure modes and damage evolution in polymeric composites and sandwich structures. [ABSTRACT FROM AUTHOR]