Health Monitoring of Aluminum Aircraft Structural Elements Using Piezoelectric Sensors
2012
Sergejs Kuzņecovs

Defending
25.01.2012. 14:30, TMF, Aviācijas institūts, Lomonosova iela 1/B B-220, Rīga

Supervisor
Vitālijs Pavelko

Reviewers
Semjons Cifanskis, Egons Lavendelis, Jurijs Paramonovs

The purpose of this work is the experimental research of some rudimentary elements of an integrated Structural Health Monitoring system which is based on piezoelectric sensors and exploits guided Lamb Waves and Electromechanical Impedance feature as physical phenomenon for damage detection in aluminum aircraft thin walled structures.


Keywords
structural health monitoring, monitoring, aircraft, piezoceramic sensors, lamb waves

Kuzņecovs, Sergejs. Health Monitoring of Aluminum Aircraft Structural Elements Using Piezoelectric Sensors . PhD Thesis. Rīga: [RTU], 2012. 158 p.

 Publication language
English (en)
  • Publication Type
    Doctoral Thesis
  • Funding for basic activity
    Unknown
  • Field of research
    2. Engineering and technology
  • Sub-field of research
    2.3 Mechanical engineering
  • ID: 12369
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