Regular-Class Airliner


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Engineering

Balsa, cedar, plastic, aluminium alloy, titanium alloy
49.2 × 120.0 × 7.8 in.

2018

The aircraft was designed as a environmental-friendly airliner.  The objective of this project is to design an aircraft that can lift as much weight as required while using the least energy.

Finite element analysis was applied to approach desired result and ensure quality under the maximun capacity.

This aircraft won the 4th place at 2018 SAE International Aero Design West




Ziming Wang

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