Abstract
This paper concerns an application of the fuzzy structures analysis (FSA) procedures of Soize to prototypical aerospace panels in MSC/NASTRAN, a large commercial finite element program. A brief introduction to the FSA procedures is first provided. The implementation of the FSA methods is then disclosed, and the method is validated by comparison to published results for the forced vibrations of a fuzzy beam. The results of the new implementation show excellent agreement to the benchmark results. The ongoing effort at NASA Langley and Penn State to apply these fuzzy structures analysis procedures to real aircraft panels is then described.
| Original language | English (US) |
|---|---|
| State | Published - Dec 1 2001 |
| Event | 19th AIAA Applied Aerodynamics Conference 2001 - Anaheim, CA, United States Duration: Jun 11 2001 → Jun 14 2001 |
Other
| Other | 19th AIAA Applied Aerodynamics Conference 2001 |
|---|---|
| Country/Territory | United States |
| City | Anaheim, CA |
| Period | 6/11/01 → 6/14/01 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Mechanical Engineering