What is it about?
The safe design of panels against aeroelastic instability is driven by the determination of critical aerodynamic conditions. We show an improved numerical strategy to tackle the aeroelastic problem using tow-steered composite panels considering a multi-criterion optimization framework and manufacturing constraints.
Featured Image
Read the Original
This page is a summary of: Supersonic Flutter and Buckling Optimization of Tow-Steered Composite Plates, AIAA Journal, January 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057282.
You can read the full text:
Contributors
The following have contributed to this page