Interaction of Lamb waves with structural features of an aircraft fuselage

Proceedings of the 5th European Workshop - Structural Health Monitoring 2010

Volumn , Issue , 2010, Pages 1347-1352

  Olson, S E ^a   Desimio, M P ^a   Swenson, E D ^b   Sohn, H ^c  

^a UNIVERSITY OF DAYTON RESEARCH INSTITUTE   (United States)

^b AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^c Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

COMPLEX GEOMETRIES; DETECTION TECHNIQUE; DOUBLERS; EXPERIMENTAL TESTING; FINITE ELEMENT SIMULATIONS; FLAT PLATE; FREQUENCY-SHIFTING; GRID POINTS; LASER DOPPLER VIBROMETERS; METALLIC STRUCTURES; MODE CONVERSIONS; OUT-OF-PLANE VELOCITY; SIMPLE GEOMETRIES; STRUCTURAL FEATURE; VIBROMETERS; WAVE FORMS;

ALUMINUM; CRACK DETECTION; ELASTIC WAVES; GEOMETRY; PLATES (STRUCTURAL COMPONENTS); STRUCTURAL HEALTH MONITORING; ULTRASONIC WAVES;

FUSELAGES;

EID: 79956216894     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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