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title: 31st Structures, Structural Dynamics and Materials Conference
ZEUS-DO: Design Oriented CFD-Based Unsteady Aerodynamics for Flight Vehicle Shape Optimization
Zero-Lift Drag Prediction Including Aeroelastic Effects (AIAA 2014-1194)
X-HALE: A Very Flexible UAV for Nonlinear Aeroelastic Tests
XFEM Toolkit for Delamination Failure Prediction of Composite Bonded Pi Joints
XFEM Toolkit for Crack Path and Life Prediction of Aluminum Structures
X-FEM for Three-Dimensional Dynamic Crack Growth
X-34 Dynamic Modeling and Correlation
X33 Transient Liftoff Analysis
X-33/RLV System Health Management/Vehicle Health Management
X-33/RLV Reusable Cryogenic Tank VHM Using Fiber Optic Distributed Sensing Technology
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
Wrinkling Analysis of a Kapton Square Membrane Under Tensile Loading
Wrinkle/Slack Control Using Shape Memory Polymer Films for Large Membrane Structures
Wrinkle Generation Mechanism without Buckling in Sheared Rectangular Membrane
Wrinkle-Crease Interaction Simulation Using Combined MT Model and DP Technique