Reduced order modeling for aero-thermo-elastic response of nonlinear panel in supersonic flow based on approximate inertial manifolds

Wei Kang1, Yang Tang1, Min Xu1, Jiazhong Zhang2

Journal of Vibration and Shock ›› 2015, Vol. 34 ›› Issue (21) : 49-53.

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PDF(1589 KB)
Journal of Vibration and Shock ›› 2015, Vol. 34 ›› Issue (21) : 49-53.

Reduced order modeling for aero-thermo-elastic response of nonlinear panel in supersonic flow based on approximate inertial manifolds

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