PDF(1589 KB)
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.
PDF(1589 KB)
PDF(1589 KB)
Reduced order modeling for aero-thermo-elastic response of nonlinear panel in supersonic flow based on approximate inertial manifolds
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