Operational modal analysis of a rotating helicopter blade

Proceedings of ISMA 2010 - International Conference on Noise and Vibration Engineering, including USD 2010

Volumn , Issue , 2010, Pages 3249-3262

  Agneni, A ^a   Coppotelli, G ^a   Grappasonni, C ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE BEAMS AND GIRDERS; FREQUENCY ESTIMATION; HARMONIC ANALYSIS; MATHEMATICAL TRANSFORMATIONS; PARAMETER ESTIMATION; SENSITIVITY ANALYSIS; STOCHASTIC SYSTEMS; STRUCTURAL DYNAMICS;

FREQUENCY INDEPENDENT; GERMAN AEROSPACE CENTERS; HARMONIC COMPONENTS; HILBERT TRANSFORMATIONS; OPERATING CONDITION; OPERATIONAL MODAL ANALYSIS; STATISTICAL CHARACTERIZATION; STATISTICAL PARAMETERS;

MODAL ANALYSIS;

EID: 84951123612     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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