High frequency surface acoustic waves under the microscope
Humboldt-Spektrum 3-4 (2004) 62
Nanoacoustics – High-Frequency Acoustic Wave Fields under the Microscope
Chapter in Science, Technology and Education of Microscopy: an Overview, Formatex 1 (2004) 9
Distribution of the dynamic strain and stress components within a layered film of A SAW resonator on LiTaO3
Proceedings of the IEEE Ultrasonics Symposium 1 (2003) 312-315
Abstract:
Based on recent reports about the acoustical power distribution in SAW resonators we present an analytical method to determine the distribution of the dynamic strain and stress components in SAW resonators on LiTaO3. This enables us to calculate the absolute strain and stress values for each point in the layer of a resonator for any driving condition and frequency. The SAW resonator is described by a P-Matrix based model, which gives us the distribution of the potential power and the resulting energy density. For calculation of the relative strain and stress values we used the Partial Wave Method. Using the correlation between the total acoustic power and the energy density distribution normal to the substrate surface, we can calculate the strain and stress values for a given input power. For the direct experimental verification of our calculations we measured the SAW induced displacements as a function of input power.Distribution of the dynamic strain and stress components within a layered film of a SAW resonator on LiTaO3
Proceedings of the IEEE Ultrasonics Symposium 2 (2003) 1149-1152
Abstract:
Based on recent reports about the acoustical power distribution in SAW resonators we present an analytical method to determine the distribution of the dynamic strain and stress components in SAW resonators on LiTaO3. This enables us to calculate the absolute strain and stress values for each point in the layer of a resonator for any driving condition and frequency. The SAW resonator is described by a P-Matrix based model, which gives us the distribution of the potential power and the resulting energy density. For calculation of the relative strain and stress values we used the Partial Wave Method. Using the correlation between the total acoustic power and the energy density distribution normal to the substrate surface, we can calculate the strain and stress values for a given input power. For the direct experimental verification of our calculations we measured the SAW induced displacements as a function of input power.In-situ study of acoustomigration by scanning Acoustic Force Microscopy
Proceedings of the IEEE Ultrasonics Symposium 2 (2003) 1483-1486