EXPERIMENTAL VALIDATION OF A STRUCTURAL HEALTH MONITORING METHODOLOGY: PART III. DAMAGE LOCATION ON AN AIRCRAFT WING
- 1 January 2003
- journal article
- Published by Elsevier BV in Journal of Sound and Vibration
- Vol. 259 (2), 365-385
- https://doi.org/10.1006/jsvi.2002.5169
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- EXPERIMENTAL VALIDATION OF A STRUCTURAL HEALTH MONITORING METHODOLOGY: PART II. NOVELTY DETECTION ON A GNAT AIRCRAFTJournal of Sound and Vibration, 2003
- EXPERIMENTAL VALIDATION OF A STRUCTURAL HEALTH MONITORING METHODOLOGY: PART I. NOVELTY DETECTION ON A LABORATORY STRUCTUREJournal of Sound and Vibration, 2003
- An Experimental Appraisal of the Strain Energy Damage Location MethodKey Engineering Materials, 2001
- DAMAGE DETECTION USING OUTLIER ANALYSISJournal of Sound and Vibration, 2000