Abstract
This paper provides a new design of a sandwich structure used in aircafts. To optimize this design, bird-strike tests are carried out on a sandwich structure made of a honeycomb core and aluminum cover plates, and a numerical model of this structure is developed with the explicit finite element program PAM-CRASH. The results of simulation, which describes the failure of the sandwich structure, agree well with test results. An improved structure is developed based on this result and bird-strike tests are carried out on the new structure. The reliability of the design is proved and the improved structure shows good behavior against bird-strikes in the tests.
Original language | English |
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Pages (from-to) | 68-76 |
Number of pages | 9 |
Journal | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
Volume | 33 |
Issue number | 1 |
State | Published - Jan 2012 |
Keywords
- Bird-strike
- Bird-strike test
- Honeycomb-based sandwich
- Numerical simulation
- PAM-CRASH