Output-only approach for finite element model updating of AB-204 helicopter blade

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 8, Issue , 2005, Pages 5587-5598

  Crema, L Balis ^a,b   Coppotelli, G ^a,b  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

^b Dipprtimento di Ingegneria Aerospaziale e Astronautica   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

FINITE ELEMENT MODELS; HELICOPTER BLADES; MODAL PARAMETERS; STRUCTURAL MODELS;

BOUNDARY CONDITIONS; CORRELATION METHODS; ERRORS; FINITE ELEMENT METHOD; FREQUENCY RESPONSE; FUNCTIONS; HELICOPTERS; MATHEMATICAL MODELS; MODAL ANALYSIS; STRUCTURAL ANALYSIS;

TURBOMACHINE BLADES;

EID: 28844468529     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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18. Balis Crema, L., Coppotelli, G., La Scaleia, B., Identification and Updating of AB204 Helicopter Blade F.E. Model by Means of Static and Dynamic Tests, 45 AIAA/ASME/ASCE/AHS/ASC, Structures, Structural Dynamics, and Materials Conference, paper No. AIAA-2004-1946 , 2004.