Absolute Nodal Coordinate Beam Element for Modeling Flexible and Deployable Aerospace Structures
Absolute Nodal Coordinate Formulation-Based Shape Sensing Approach for Large Deformation: Plane Beam
Accurate Stick Model Development for Static Analysis of Complex Aircraft Wing-Box Structures
Aerodynamic Load Estimation from Virtual Strain Sensors for a Pliant Membrane Wing
Aeroelastic Analysis of Wing Structures Using Equivalent Plate Models
Aeroelastic Demonstrator Wing Design for Maneuver Load Alleviation Under Cruise Shape Constraint
Aeroelastic Simulations of High Reynolds Number Aero Structural Dynamics Wind Tunnel Model
Aero-Optical Measurements of the Response of a Thin Panel at Mach 6
An Algebraic Model for Structural and Life Analysis of Regeneratively-Cooled Thrust Chambers
Analysis of Constrained Damping Layers, Including Normal-Strain Effects
Analysis of Functionally Graded Plates Subjected to Hygrothermomechanical Loads
Analysis of Laminated Plates by Trigonometric Theory, Radial Basis, and Unified Formulation
Analytical Investigation on Elastic–Plastic Deformation of Reentrant Honeycomb Structures
Analytical Model for Transverse Vibrations of Spinning Membranes
Analytical Solution for Buckling Analysis of Composite Cylinders with Honeycomb Core Layer
Assessment of Beam and Shell Elements for Modeling Rotorcraft Blades
Assessment of Composite and Sandwich Laminates Using a New Shear Deformation Theory