SearcharxivSearch

arXiv subjects

Martin Schagerl

Publications and source records attributed to Martin Schagerl.

2 recordsLinked to original sources

Single-shot capable surface acoustic wave dispersion measurement of a layered plate

Established techniques for characterizing a layer on a substrate system via surface acoustic wave (SAW) dispersion measurement are often slow due to the need for scanning excitation or detection positions. We present a method for determining discrete points on the SAW mode at equidistant wavenumbers that requires only a single measurement, overcoming these speed limitations. A pulsed laser, shaped into an array of equidistant lines, generates elastic waves on the sample surface. A vibrometer detects the resulting surface displacement next to the line array. The periodic excitation arrangement results in constructive interference of the SAW at wavelengths corresponding to integer fractions of the line spacing. This leads to distinct peaks in the response spectrum, whose higher orders we term spatial harmonics of the SAW. The known line spacing determines the wavelengths, allowing the peak frequencies to be mapped to discrete points on the SAW dispersion curve, effectively sampling the SAW at specific equidistant wavenumbers. By solving an inverse problem, a model can be fit to the experimental data to obtain properties of the layered system. We demonstrate this technique on copper-clad epoxy laminate and roll-cladded aluminum alloy plates and compare our results with dispersion relation scans and micrography. Additionally, we analyze the method's sensitivity to elastic parameters and layer thickness. This approach offers a viable alternative to established SAW scanning methods, particularly in scenarios where the trade-off of lower wavenumber sampling density is acceptable to achieve exceptionally fast measurements while avoiding moving parts.

cond-mat.mtrl-sci

Development of Aircraft Spoiler Demonstrators for Cost-Efficient Investigations of SHM Technologies under Quasi-Realistic Loading Conditions

An idealized 1:2 scale demonstrator and a numerical parameter optimization algorithm are proposed to closely reproduce the deformation shape and, thus, spatial strain directions of a real aerodynamically loaded civil aircraft spoiler using only four concentrated loads. Cost-efficient experimental studies on demonstrators of increasing complexity are required to transfer knowledge from coupons to full-scale structures and to build up confidence in novel structural health monitoring (SHM) technologies. Especially for testing novel sensor systems that depend on or are affected by mechanical strains, e.g., strain-based SHM methods, it is essential that the considered lab-scale structures reflect the strain states of the real structure at operational loading conditions. Finite element simulations with detailed models were performed for static strength analysis and for comparison to experimental measurements. The simulated and measured deformations and spatial strain directions of the idealized demonstrator correlated well with the numerical results of the real aircraft spoiler. Thus, using the developed idealized demonstrator, strain-based SHM systems can be tested under conditions that reflect operational aerodynamic pressure loads, while the test effort and costs are significantly reduced. Furthermore, the presented loading optimization algorithm can be easily adapted to mimic other pressure loads in plate-like structures to reproduce specific structural conditions.

cs.CE