A Probabilistic Approach in Fuselage Damage Analysis <em>via</em> Boundary Element Method
This chapter presents a new alternative approach to the analysis of the fatigue life of aircraft fuselage parts considering the compliance of internal elements to replace the classical model of critical crack size. In this case, from a global–local analysis using the boundary element method (BEM), i...
Guardado en:
| Autores principales: | , , |
|---|---|
| Formato: | Capítulo de libro |
| Lenguaje: | inglés |
| Publicado: |
IntechOpen
2021
|
| Materias: | |
| Acceso en línea: | https://www.intechopen.com/chapters/77541 |
| Etiquetas: |
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
Ejemplares similares: A Probabilistic Approach in Fuselage Damage Analysis <em>via</em> Boundary Element Method
- Aircraft Fuselage Defect Detection using Deep Neural Networks
- Quantum Safe-Set Bayesian Optimization for Quality Improvement in Fuselage Assembly
- Active Learning for Gaussian Process Considering Uncertainties with Application to Shape Control of Composite Fuselage
- SAPO-RL: Sequential Actuator Placement Optimization for Fuselage Assembly via Reinforcement Learning
- A Robust Sustainability Assessment Methodology for Aircraft Parts: Application to a Fuselage Panel
- Efficient solution strategies for cabin noise assessment of a wave resolving aircraft fuselage model