Reduced-Order Models for Acoustic Response Prediction of a Curved Panel
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2081
Reference15 articles.
1. 1McEwan, M.I., Wright, J.R., Cooper, J.E., and Leung, A.Y.T. "A Finite Element/Modal Techniquefor Nonlinear Plateand StiffenedPanel ResponsePrediction,"AIAA-2001-1595,2001.
2. Nonlinear modal models for sonic fatigue response prediction: a comparison of methods
3. 4Gordon, R.W., and Hollkamp, J.J. "Nonlinear Random Response of a Clamped Plate: A Well-Characterized Experiment," AIAA-2006-1924,2006.
4. Nonlinear Reduced Order Random Response Analysis of Structures with Shallow Curvature
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