Analytical modeling to develop SHM techniques for aircraft "hot spots"

Structural Health Monitoring 2007: Quantification, Validation, and Implementation - Proceedings of the 6th International Workshop on Structural Health Monitoring, IWSHM 2007

Volumn 2, Issue , 2007, Pages 2041-2048

  Olson, S E ^a   Leonard, M S ^b   Malkin, M C ^c  

^a UNIVERSITY OF DAYTON RESEARCH INSTITUTE   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CRACKS; DAMAGE DETECTION; ELASTIC WAVES; FATIGUE DAMAGE; FIGHTER AIRCRAFT; FINITE ELEMENT METHOD; SURFACE WAVES; WAVE PROPAGATION;

AEROSPACE STRUCTURE; AIRCRAFT STRUCTURAL COMPONENTS; COMPLICATED STRUCTURES; DETECTION CAPABILITY; MODELING TECHNIQUE; PROPAGATION BEHAVIOR; STRUCTURAL HEALTH MONITORING (SHM); SYSTEM CONFIGURATIONS;

STRUCTURAL HEALTH MONITORING;

EID: 84866702997     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (2)

1. Kusaka. T and Qing. P. 2003. 'Characterization of loading effects on the performance of SMART layer embedded or surface-mounted on structures," Proceedings of the 4th International Workshop on Structural Health Monitoring. September 15-17. 2003, pp 1539 1546.
2. ABAQUS Analysis User's Manual. Version 6.5. 2005. Providence. Rl: ABAQUS Inc.