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Lightweight and Efficient Manifold Design for Hydrogen Fuel Cell Powered Unmanned Aerial Vehicles (UAVs)

Stichwort:

multi-jet fusion printing, manifold, hydrogen fuel cell, Unmanned Aerial Vehicles, proton exchange membrane, and design optimization

Schöpfer:

Islam, Sophia, Purtell, Avery, Bonito, Michael, Cassidy, Jack, and Hemmerling, Liam

Advisor:

Sabuncu, Ahmet Can

Herausgeber:

Worcester Polytechnic Institute

Datum erstellt:

2024-04-23

Resource Type:

Major Qualifying Project