Identification of a nonlinear wing structure using an extended modal model

Journal of Aircraft

Volumn 46, Issue 5, 2009, Pages 1614-1626

  Platten, M F ^a   Wright, J R ^b,c   Cooper, J E ^d,e   Dimitriadis, G ^f,g  

^a Romax Technology Limited   (United Kingdom)

^b UNIVERSITY OF MANCHESTER   (United Kingdom)

^c George Begg Building

^d UNIVERSITY OF LIVERPOOL   (United Kingdom)

^e Department of Engineering ^*

^f UNIVERSITY OF LIÈGE   (Belgium)

^g Aerospace and Mechanical Engineering Department

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); LINEAR SYSTEMS; NONLINEAR DYNAMICAL SYSTEMS;

DEGREE OF FREEDOM; EXPERIMENTAL APPLICATION; GROUND VIBRATION TESTING; NON-LINEAR RESONANT DECAY METHODS; NONLINEAR BEHAVIOR; RECTANGULAR WINGS; RESTORING FORCE SURFACES; STRONGLY NONLINEAR;

WINGS;

EID: 73649098501     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.42024     Document Type: Article

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