Prediction of the non-linear response of a clamped panel to acoustic loading

Proceedings of the 2004 International Conference on Noise and Vibration Engineering, ISMA

Volumn , Issue , 2004, Pages 3671-3685

  Acton, M N F ^a   Platten, M F ^a   Wright, J R ^a   Cooper, J E ^a   Olsson, A ^b  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

^b BAE SYSTEMS   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; COSTS; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; JET ENGINES; STRUCTURAL PANELS; TIME DOMAIN ANALYSIS;

ACOUSTIC EXCITATION; ACOUSTIC LOADING; CLAMPED PANELS; STRESS RESPONSE;

ACOUSTIC WAVE EFFECTS;

EID: 13344280318     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

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2. Rizzi, S.A., Muravyov, A.A., Equivalent Linearization of Geometrically Nonlinear Random Vibrations Using Commercial Finite Element Codes, NASA/TP-2002-211761, 2002
3. Shi, Y., Mei, C., A Finite Element Time Domain Model Formulation for Large Amplitude Free Vibrations of Beams and Plates, J. Sound and Vibration, 193(2), 453-464, 1996.
4. nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 2001
5. McEwan, M.I., A Combined Modal/Finite Element Technique For the Nonlinear Dynamic Simulation of Aerospace Structures, PhD Dissertation, Univ. of Manchester, England, 2001.
6. th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Norfolk, Virginia, 2003.