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.
Fuzzy Structures Analysis of Aircraft Panels in NASTRAN
2001-01-01
Preprint
No indication
English
Fuzzy Structures Analysis of Aircraft Panels in NASTRAN
NTIS | 2001
|Fuzzy structures analysis of aircraft panels in NASTRAN
AIAA | 2001
|AIAA-2001-1320 Fuzzy Structures Analysis of Aircraft Panels in NASTRAN
British Library Conference Proceedings | 2001
|Structural analysis of light aircraft using NASTRAN
AIAA | 1974
|Structural analysis of light aircraft using NASTRAN
NTRS | 1973
|