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Werkstoff
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Monitoring Strain Rate Effects on Nanocomposites using Piezospectroscopy (AIAA 2014-0109)
Reliability aspects of microsystems for automotive applications
Pileup Investigation on Work Hardened Copper During Sharp Tip Nanoindentation (AIAA 2014-1330)
A Flutter Analysis Procedure Applicable to Conceptual Design (AIAA 2014-1195)
Lyapunov Stability Analysis of an Aeroleastic Torsion Model (AIAA 2014-1043)
The Use of the STAGS Finite Element Code in Stitched Structures Development (AIAA 2014-0845)
Tracking Design Evolution in Aircraft Structural Modeling (AIAA 2014-0216)
Reduced Order Modeling for the Nonlinear Geometric Response of Some Joined Wings (AIAA 2014-0151)
Satellite Technology & Applications: Course Development and Implementation (AIAA 2014-0061)
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)
Modeling of Plain Woven Fabrics for Inflatable Aerodynamic Decelerators (AIAA 2014-0631)
Hyperion - Three Years of Novel Aircraft Design (AIAA 2014-0575)
Aeroelastic Tailoring of a Plate Wing with Functionally Graded Materials (AIAA 2014-0344)
Optimisation of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring (AIAA 2014-0343)
An Aircraft Design Competition for High School STEM Improvement (AIAA 2014-0063)
Water Management Strategy for the PEM Fuel Cell
Hierarchical Analysis and Optimization of Nano-Enhanced Composite Sandwich Plates (AIAA 2014-1377)
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)