AIAA-2004-2043 Nonlinear Flutter of Cylindrical Shell Panels Under Yawed Supersonic Flow Using FE
AIAA-2006-1745 Dynamic Snap Through of Thin-Walled Structures by a Reduced Order Method
Analysis of a Hybrid Wing Body Center Section Test Article
Comparison of PDE/Galerkin and FEM for Non-linear Aerospace Structure Analyses
Design and Analysis of a Stiffened Composite Structure Repair Concept
Energy-Based Modal Basis Selection Procedure for Reduced-Order Nonlinear Simulation
Multimode Large Amplitude Free Vibration of Shallow Shells Considering Inplane Inertia
Nonlinear Flutter of Curved Panels Under Yawed Supersonic Flow Using Finite Elements
Nonlinear Reduced-Order Analysis with Time-Varying Spatial Loading Distributions
Nonlinear Reduced-Order Simulation Using an Experimentally Guided Modal Basis
Nonlinear Reduced-Order Simulation Using Stress-Free and Pre-Stressed Modal Bases
Nonlinear Response and Fatigue Life of Shallow Shells to Acoustic Excitation Using Finite Element