In the field of aeronautics (Aircraft, helicopters, space launchers...), as in the field of the automobile, reducing the harmful effects of acoustics constitutes a major concern at the international level and justifies the call for further research. With these challenges in mind, the manufacturers have expressed the need for simple models immediately available as early as the stage of preliminary drafts. This Master's Thesis presents the study and the validation of three different approaches to meet this industrial need. The first approach is based on the propagation of waves in the structure; the second approach uses the technique of SEA by calculating the equivalent damping; and the last approach uses the modal technique.In the three approaches, the transfer matrix method has been used to study the succession of layers. Applying these approaches to some aircraft structures confirm their relevance in relation to more exact and costly methods, such as the finite elements method.
| Identifer | oai:union.ndltd.org:usherbrooke.ca/oai:savoirs.usherbrooke.ca:11143/1409 |
| Date | January 2007 |
| Creators | Rhazi, Dilal |
| Contributors | Atalla, Noureddine |
| Publisher | Université de Sherbrooke |
| Source Sets | Université de Sherbrooke |
| Language | French |
| Detected Language | English |
| Type | Mémoire |
| Rights | © Dilal Rhazi |
Page generated in 0.0023 seconds