Optimisation of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring
Author:
Affiliation:
1. University of Bristol
2. Airbus
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0343
Reference38 articles.
1. Aeroelastic tailoring of forward swept composite wings
2. Aeroelastic tailoring - Theory, practice, and promise
3. Aeroelastic Tailoring of Composite Structures
4. Induced Drag Reduction Using Aeroelastic Tailoring with Adaptive Control Surfaces
5. Optimization of a Wing Structure for Gust Response and Aileron Effectiveness
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2. Effects of Sweep Angle in Aeroelastic Response of Wings Made of Isotropic and Fiber Reinforced Composite Materials;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07
3. Economical Unsteady High Fidelity Aerodynamics in a Structural Optimization with a Flutter Constraint;35th AIAA Applied Aerodynamics Conference;2017-06-02
4. On the Interpretation of Bending-Torsion Coupling for Swept, Non-Homogenous Wings;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02
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