A study on vibration-based damage detection and location in an aircraft wing scaled model

Applied Mechanics and Materials

Volumn 3-4, Issue , 2005, Pages 309-314

  Trendafilova, I ^a  

^a UNIVERSITY OF STRATHCLYDE   (United Kingdom)

Author keywords

Aircraft wing FE modelling; Modal frequencies; Mode shapes; Structural damage detection; Structural vibration response

Indexed keywords

FINITE ELEMENT METHOD; MATHEMATICAL MODELS; MODAL ANALYSIS; VIBRATIONS (MECHANICAL);

AIRCRAFT WING FE MODELING; MODAL FREQUENCIES; MODE SHAPES; STRUCTURAL DAMAGE DETECTION; STRUCTURAL VIBRATION RESPONSE;

WINGS;

EID: 33745160046     PISSN: 16609336     EISSN: 16627482     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/AMM.3-4.309     Document Type: Conference Paper

References (6)

1. H.J. Schmidt, J. Telgkamp and B. Schmidt-Brandecker: Structural Health Monitoring 2004, Proc. of the II European Workshop, p. 11
2. C.A.Paget and K.J.Aherton: Structural Health Monitoring 2004, Proc. of the II European Workshop, p382.
3. S.W.Doebling, C.R. Farrar and M.B. Prime: Shock and Vibration Digest, vol.205(5), (1998), p 631.
4. P. Verboven, E. Parloo, P. Guillaume and M. Van Overmeire: Mechanical Systems and Signal Processing, vol. 16(4), (2002), p.637.
5. B.Lazarov and I.Trendafilova: Structural Health Monitoring 2004, Proc. of the II European Workshop, p.76
6. D.J. Ewins: Modal Testing theory practice and application (Research Studies Press LTD 2000).