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Jan 2025 – Present -
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Mar 2024 – Dec 2024 -
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Oct 2021 – Sep 2023 -
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Jul 2022 – Sep 2022 -
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Feb 2022 – Apr 2022 -
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Objective — Design and validate CFRP panels with stringers, minimizing weight while meeting buckling and damage-tolerance requirements under the defined load cases.

What I did
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Objective — Simulate a UD laminate under tension and compression using Hashin damage initiation to identify ply-by-ply failure and compare tensile vs compressive capacity.

Model
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Objective — Define composite skin and stringer concept, reinforcements, drop-offs, and frame joints (clips, Ø4.8 mm) for a fuselage bay between Frames A–B.

Given data
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  • Defined clip joints and prepared drawings, materials list, and panel weight.

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      Objective — Design the lightest possible rear saddle frame within the boundary envelope, load-case compliant (static + fatigue), manufacturable by SLM (AlSi10Mg).

      Process
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    • Final weight: ~656 g after combined-load map optimization.

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      Objective — Define laminate schedule and thicknesses to minimize weight while maintaining stiffness and strength on a composite drone frame, with harmonic and impact checks on critical members.

      What I did
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    • Local reinforcements added only where needed after impact assessment.

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      Oct 2024 – Jun 2025 -
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      Oct 2022 – Dec 2025 / Mar 2026 -
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      Sep 2023 – Feb 2024 -
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      Sep 2019 – Oct 2022 -
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