2 research outputs found
Quantum Neural Networks for Power Flow Analysis
This paper explores the potential application of quantum and hybrid
quantum-classical neural networks in power flow analysis. Experiments are
conducted using two small-size datasets based on the IEEE 4-bus and 33-bus test
systems. A systematic performance comparison is also conducted among quantum,
hybrid quantum-classical, and classical neural networks. The comparison is
based on (i) generalization ability, (ii) robustness, (iii) training dataset
size needed, (iv) training error. (v) training computational time, and (vi)
training process stability. The results show that the developed
quantum-classical neural network outperforms both quantum and classical neural
networks, and hence can improve deep learning-based power flow analysis in the
noisy-intermediate-scale quantum (NISQ) era.Comment: 7 pages, 15 figure
C<sup>1</sup> Cohesive Element Models for 3D Delamination: Towards overcoming the mesh density constraint in FE delamination analyses
The wide adoption of composite structures in the aerospace industry asks for reliable numerical methods to account for the effects of damage, among which delamination. Cohesive elements (CEs) are a versatile and physically representative way of reproducing delamination, but, using their standard form, at least 3 elements are required in the narrow cohesive zone, hindering the applicability in practical scenarios. This limitation is due to the inability ofcurrent models to capture the deformation of the delaminating substrates. The present work focuses on the implementation and testing of triangular thin plate substrate elements and compatible cohesive elements, which satisfy C1-continuity at their boundary. The improved regularity meets the continuity requirement coming from the Kirchhoff Plate Theory and the triangular shape allows for conformity to complex geometries. After verification of plate andcohesive element singularly, the overall model is validated for mode I delamination. Very accurate predictions of the limit load and crack propagation phase are found, using CEs as large as 11 times the cohesive zone.Aerospace Engineerin