Towards Crash-Tolerant Rotorcraft Design via Topology Optimization

F-0081-2025-0232

5/20/2025

Authors
Abstract
Content
ABSTRACT

We present our ongoing efforts towards the development of crash-tolerant rotorcraft airframe structures through topology optimization, with the goal of enhancing energy absorption and occupant survival during vertical impact events. A high strain rate explicit dynamics solver has been developed, fully accelerated on GPUs, to enable rapid and accurate simulation of impact events critical to crashworthiness evaluation. In parallel, we have built a scalable three-dimensional topology optimization framework that enforces stiffness, weight, and frequency constraints simultaneously, driving structurally efficient and vibration-resistant designs. Benchmarking results demonstrate significant GPU-enabled speedups, facilitating high-fidelity crash simulations and large-scale optimization at practical turnaround times. This work establishes a computational foundation for future integration of crash-centric objectives and constraints into the optimization framework.

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DOI
https://doi.org/10.4050/F-0081-2025-0232
Citation
Das, G., James, K., Kennedy, G., Webb, L., et al., "Towards Crash-Tolerant Rotorcraft Design via Topology Optimization," Vertical Flight Society 81st Annual Forum and Technology Display, Virginia Beach, Virginia, May 20, 2025, https://doi.org/10.4050/F-0081-2025-0232.
Additional Details
Publisher
Published
5/20/2025
Product Code
F-0081-2025-0232
Content Type
Technical Paper
Language
English