This paper concerns the second phase of an experimental validation programme for a structural health monitoring methodology based on novelty detection. This phase seeks to apply one of the methods considered in the first stage of the work on a more realistic structure, namely the wing of a Gnat airc
โฆ LIBER โฆ
EXPERIMENTAL VALIDATION OF A STRUCTURAL HEALTH MONITORING METHODOLOGY: PART III. DAMAGE LOCATION ON AN AIRCRAFT WING
โ Scribed by G. MANSON; K. WORDEN; D. ALLMAN
- Publisher
- Elsevier Science
- Year
- 2003
- Tongue
- English
- Weight
- 501 KB
- Volume
- 259
- Category
- Article
- ISSN
- 0022-460X
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๐ SIMILAR VOLUMES
EXPERIMENTAL VALIDATION OF A STRUCTURAL
โ
G. MANSON; K. WORDEN; D. ALLMAN
๐
Article
๐
2003
๐
Elsevier Science
๐
English
โ 509 KB
EXPERIMENTAL VALIDATION OF A STRUCTURAL
โ
K. WORDEN; G. MANSON; D. ALLMAN
๐
Article
๐
2003
๐
Elsevier Science
๐
English
โ 420 KB
This paper is concerned with the experimental validation of a structural health monitoring methodology, previously only investigated using synthetic data. The structure considered here is a simplified model of a metallic aircraft wingbox i.e., a plate incorporating stiffening elements. Damage is sim