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Werkstoff
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Zero-Lift Drag Prediction Including Aeroelastic Effects (AIAA 2014-1194)
A Computational Model for the Flow of Resin in Self-Healing Composites (AIAA 2014-0849)
Multi-scale Intrinsic Flaws in Composite Materials (AIAA 2014-0798)
Computational Transonic Flutter Solutions for Cranked Wing Planforms (AIAA 2014-0674)
Design and Optimization of Opencell™ Metal Sandwich Cylindrical Panel (AIAA 2014-0502)
A Three-Dimensional Multi-Stable Unit Cell for Energy Dissipation (AIAA 2014-0501)
An Approach for Evaluating Potential Aircraft Casualties from Combat Threats (AIAA 2014-0354)
R: An Opensource System for Statistics and Data Exploration (AIAA 2014-0349)
Where Open Source FEA Fits in the CAE Ecosystem and What to Know Before Adopting (AIAA 2014-0347)
Higher-Order Transonic Flutter Solutions (AIAA 2014-0336)
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)
Aeroelastic Wing Shaping Control Subject to Actuation Constraints (AIAA 2014-1041)
Implementation of the CUDA Cusp and CHOLMOD Solvers in CalculiX (AIAA 2014-0346)
Calculation of Equivalent Initial Flaw Size Distributions for Multiple Site Damage (AIAA 2014-1526)
The Use of Relational Design in Aircraft Product Development (AIAA 2014-1207)
Flight Loads Spectra of Two Business Jets (AIAA 2014-1206)
Modelling the High Temperature Fatigue Behaviour of Titanium Alloys (AIAA 2014-0994)