Crashworthiness Design with Bending Optimization in the Hybrid Cellular Automata Framework: A Design Methodology for Aircraft Sub-Floor Structures

Structural design for unconventional aircraft can be quite challenging and could undergo<br/>many iterations until a solution is found for all load-cases such as static sizing, stability and<br/>crashworthiness. Ultimately, all of the design aspect are integrated in the earliest design<br/>changes for which Topology Optimization (TO) could...