Numerical simulation for random aeroelastic responses using inverse fourier transform

This paper reports a new simulation technique for an aeroelastic system which responds to random external forces. Since the aeroelastic system including the effects of unsteady aerodynamics is ordinarily described in the frequency domain, the Inverse Discrete Fourier Transform (IDFT) can be utilized to simulate its random response. The response caused by the external random noise is calculated through a transfer function first in the frequency domain and then converted to the time domain. The objective of the present study is to provide mathematical time history data for evaluating the various estimation methods of the flutter boundary from subcritical responses in flight and/or wind tunnel testing. An example application to the method of flutter prediction is shown. The technique can also be used to evaluate the effects of the active control device coping with atmospheric turbulence

Test of High Temperature Superconducting REBCO Coil Assembly for a Multi-Frequency ECR Ion Source

Chong T.H., Fukuda M., Yorita T., et al. Test of High Temperature Superconducting REBCO Coil Assembly for a Multi-Frequency ECR Ion Source. IEEE Transactions on Applied Superconductivity 34, 1 (2024); https://doi.org/10.1109/TASC.2024.3360935.High temperature superconducting REBCO tape has the characteristic of maintaining high critical current density under strong external magnetic field, which makes it an ideal material for the construction of air-core electromagnets of accelerator and electron cyclotron resonance (ECR) ion source. In Research Center for Nuclear Physics, Osaka University, a non-insulated air-cored REBCO coil assembly has been constructed. This coil assebmly consists of three circular REBCO solenoid and six racetrack REBCO coil. This coil assembly will be used as an electromagnet of a multi-frequency ECR ion source, and is also developed as a key technology development of an air-core cyclotron. The magnetic field of this ion source are designed, and 77 K performance tests of the assembly are carried out in order to examine the capability of REBCO coils of inducing magnetic field under external field. In this work, the test results and the magnetic field designed for the ECR ion source will be presented and discussed

Deformation of a Beam with Partially Debonded Piezoelectric Actuators

A linear and a non-linear mathematical models for analyzing the deformation behavior of a beam with a pair of partially debonded piezoelectric actuators are developed on the basis of the Timoshenko beam theory. Effect of buckling is considered in the linear model, where the debonded actuator region is assumed to generate the Euler buckling load when the axial force in the region is larger than the load. The static behavior of the beam is investigated for extension and bending deformation. When the actuator debonds from its edge, the performance deteriorates; in contrast, the debonding in the middle of the actuator does not show any performance degradation until the debonded region buckles. The deformation behavior obtained from the linear model has been found to have good agreement with that from the non-linear model. The non-linear analysis shows that after the buckling the debonded actuator region maintains an axial force of the order of the Euler buckling load of a fix�fix column for the extending actuation, although for the bending actuation, it retains nearly 75% of the Euler buckling load. Further, the strain distribution in the debonded region shows that the buckling may occur before cracks begin in the actuator