Key work
- Parametric FE for wing-boom-rotor integration trades.
- Primary-structure mass roll-up with growth allowance.
- Material and joining-method down-selection.
- Feasibility-report inputs on structural risk and certification basis.
2019 — 2020
Conceptual structural sizing of an e-VTOL military cargo platform: load-path layout, primary-mass estimation and material down-selection feeding the platform feasibility gate.