Methods for refinement of structural finite element models: Summary of the garteur AG14 collaborative programme

National Aerospace Laboratory NLR - 32nd European Rotorcraft Forum, ERF 2006

Volumn 2, Issue , 2007, Pages 879-906

  Hatch, C ^a   Skingle, G W ^a   Greaves, C H ^a   Lieven, N A J ^b   Coote, J E ^b   Friswell, M I ^b   Mottershead, J E ^c   Shaverdi, H ^c   Mares, C ^d   McLaughlin, A ^e   Link, M ^f   Piet Lahanier, N ^g   Van Houten, M H ^h   Goege, D ⁱ   Rottmayr, H ^j  

^a QINETIQ   (United Kingdom)

^b UNIVERSITY OF BRISTOL   (United Kingdom)

^c UNIVERSITY OF LIVERPOOL   (United Kingdom)

^d BRUNEL UNIVERSITY   (United Kingdom)

^e Westland Helicopters Ltd   (United Kingdom)

^f UNIVERSITY OF KASSEL   (Germany)

^g ONERA   (France)

^h NLR   (Netherlands)

ⁱ GERMAN AEROSPACE CENTER DLR   (Germany)

^j ECD   (Germany)

more..

Author keywords

Finite element model; Modal test; Model updating; Structural dynamics; Vibration

Indexed keywords

AEROSPACE INDUSTRY; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; STRUCTURAL DYNAMICS; VIBRATION ANALYSIS;

MODAL TESTS; VIBRATION DESIGNS; VIBRATION LEVELS;

HELICOPTERS;

EID: 34547637222     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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