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Werkstoff
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keywords:(Werkstoff)
Leichtbau durch Miniaturisierung von Komponenten, Bauteilen und Systemen
Mechanical Behaviour of Butt Jointsunder Traction Using the Image Stereocorrelation Technique
A Study on Damping of Laminated Beams by Modal Analysis
Study of Wear Properties of In Situ TiB/TiC Reinforced Ti1100 Composites
Research and Classification of Inflatable Space Vehicle and its Materials
Failure Analysis of a Helicopter's Main Rotor Bearing
Failure of the Pressure Bulkhead of a Passenger Aircraft - A Case Study
A Structural Dynamics Analysis Methodology for Development of Earth Entry Vehicles (AIAA 2014-1521)
Relationships between Nonlinear Normal Modes and Response to Random Inputs (AIAA 2014-1514)
A Thermodynamically Consistent Cohesive Zone Model for Mixed-Mode Fracture (AIAA 2014-1378)
Multi-Scale Crystal Plasticity FEM Approach to Modeling Nickel-Based Superalloys (AIAA 2014-0796)
Aeroelastic Response of Bird-Damaged Fan Blades Using a Coupled CFD/CSD Framework (AIAA 2014-0334)
Analysis of Space Structures Subject to Hypervelocity Impact (AIAA 2014-0156)
Aerothermoelastic Simulation of Air-Breathing Hypersonic Vehicles (AIAA 2014-0149)
Combining Topology and Lamination Parameter Optimisation (AIAA 2014-1372)
Nonlinear Modeling and Analysis of Wind Turbine Blades (AIAA 2014-1370)
Time-Dependent Behavior of High Strength Kevlar and Vectran Webbing (AIAA 2014-1328)
Advanced Grid-Stiffened Composite Shells for Heavy-Lift Helicopter Blade Spars (AIAA 2014-1062)
Microvascular Composite Skin Panels for Hypersonic Aircraft (AIAA 2014-0630)
Optimization of Mechanism Design of Flapping Wing MAV (AIAA 2014-0573)
Finite Element Structural Updating using FRFs (AIAA 2014-0492)
Buckling Analysis of Curvilinearly Stiffened Composite Panels with Cracks (AIAA 2014-0165)
Modeling Crack Propagation within a Reduced- Order Model Framework (AIAA 2014-0150)
Delamination Arrest by Multiple Fasteners in Bonded Composite Structures (AIAA 2014-1534)
Development of a Framework for Study of Fluid-Thermal-Elastic-Plastic Interactions (AIAA 2014-1516)
Validation of Crack Growth Analysis Technique for a Fiber Metal Laminate (AIAA 2014-1382)
Crack Arrestment of Pi-Joined Bonded Composites (AIAA 2014-1380)