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