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title: 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
XFEM Toolkit for Delamination Failure Prediction of Composite Bonded Pi Joints
XFEM Toolkit for Crack Path and Life Prediction of Aluminum Structures
X-34 Dynamic Modeling and Correlation
X33 Transient Liftoff Analysis
X-31A flight flutter test excitation by control surfaces
Wrinkling of an Inflated Membrane with Thermo-Elastic Boundary Restraint
Wrinkling Analysis Using Improved Dynamic Relaxation Method AIAA Paper 2007-2350 CD-ROM Number 8
Wrinkle/Slack Control Using Shape Memory Polymer Films for Large Membrane Structures
Wrinkle Generation Mechanism without Buckling in Sheared Rectangular Membrane
Wrinkle and Collapsing Process of Inflatable Tubes Under Bending Loads by Finite Element Analyses
Wing-Tail Interaction Flutter Revisited
Wing-tail interaction flutter revisited
Wing flutter boundary prediction using unsteady Euler aerodynamic method
Wing design for a civil filt-rotor transport aircraft: A preliminary study
Wing Design as a Symphony of Geographically Dispersed, Multi-disciplinary Undergraduate Students
Wind Turbine Blade Structural Efficiency
Wind Tunnel Test of a Very Flexible Aircraft Wing