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Werkstoff
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Adhesive Failure in Hybrid Double Cantilever Beams by Digital Image Correlation
AIAA-2001-1490 Optimum Design for Double-Lap Bolted Composite Joints Using a Genetic Algorithm
AIAA-2004-1559 Global-Local Finite Element Analysis of Bonded Single-Lap Joints
AIAA-2004-1560 Nonlinear Analysis of Bonded Composite Single-Lap Joints
AIAA-2004-1840 Three-Dimensional Analysis of Sandwich Panels with Common Defects
AIAA-2006-1662 Nonlinear Deformations of Flapping Wings on a Micro Air Vehicle
AIAA-2006-1963 Thermo-Mechanical Analysis of Bonded Cylindrically Curved Composite Shell Structures
AIAA-2006-2008 Transient Response of Composite Sandwich Panels Subjected to Blast Wave Pressure
AIAA-2006-2267 Analysis of Brazed Single-Lap Joints by Peridynamics Theory
AIAA-2006-2270 Validated Analysis Method for Bolted Composite Lap Joints
Analysis of Bolted-Bonded Composite Lap Joints AIAA Paper 2007-2187 CD-ROM Number 7
Analysis of Bolted Laminates of Varying Thickness and Lay-Up with Metallic Inserts
An Analytical Method for Evaluating Bolted Joint Repairs in Composite Structures
An Analytical Method for Evaluating Repairs in Composite Honeycomb Structure
A Refined and Efficient Approach for Dynamic Analysis of Helicopter Blades
Comparison of XFEM, CZM and PD for Predicting Crack Initiation and Propagation
Coupling of Peridynamic Theory and Finite Element Method
Effect of Core Termination Features on Failure Modes in Sandwich Panels by Using Peridynamic Theory
Fracture Behavior of Nanostructured Materials through Peridynamic Theory
Fully Coupled Peridynamic Thermomechanics
Nonlinear Analysis of a Bonded Patch Repair of a Skin with a Cutout
Ordinary State-Based Peridynamic Material Constants
Peridynamics Based on the Principle of Virtual Work
Peridynamics Damage Prediction in Composites due to Compression after Impact (AIAA 2014-1525)
Peridynamics for Failure Prediction in Composites
Post-buckling Response of Scarf Repaired Laminates Using a Refined Zigzag Element (AIAA 2014-0847)
Progressive Damage in Composite Laminates Using a Higher Order Element
Refinements in Digital Image Correlation Technique to Extract Adhesive Strains in Lap Joints
Vibration of Sandwich Panels Using {3,2}-Order Plate Theory AIAA Paper 2007-2382 CD-ROM Number 8
Wind Tunnel Tests to Modify a Drag-Type Vertical Axis Wind Turbine