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Validation of reduced order modeling for the prediction of the response and fatigue life of panels subjected to thermo-acoustic effects
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Southampton, United Kingdom, Jul. 14-16
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Prediction of the dynamic response and fatigue life of panels subjected to thermo-acoustic loading
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Honolulu, Hawaii, Apr. 23-26 AIAA Paper AIAA-2007-2014
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Continuous dynamic simulation of nonlinear aerodynamic/nonlinear structure interaction (NANSI) for morphing wing aeroelasticity
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Palm Springs, California, May 4-7 AIAA Paper AIAA-2009-2572
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Liu, D.D., Chen, P.C., Zhang, Z., Wang, Z., Yang, S., Lee, D.H., Mignolet, M.P., Kim, K., Liu, F., Lindsley, N., and Beran, P., "Continuous Dynamic Simulation of Nonlinear Aerodynamic/Nonlinear Structure Interaction (NANSI) for Morphing Wing Aeroelasticity," Proceedings of the 50th Structures, Structural Dynamics, and Materials Conference, Palm Springs, California, May 4-7, 2009. AIAA Paper AIAA-2009-2572.
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Nonlinear aeroelastic methodology for A membrane-on-ballute model with hypersonic bow shock
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Nonlinear reduced order models for thermoelastodynamic response of isotropic and FGM panels
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Perez, R., Wang, X.Q., and Mignolet, M.P., "Nonlinear Reduced Order Models for Thermoelastodynamic Response of Isotropic and FGM Panels," AIAA Journal, Vol. 49, No. 3, pp. 630-641, 2011.
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Orlando, Florida, April 12-15 AIAA Paper AIAA-2010-2724
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