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Polymer-Elektrolytmembran-Brennstoffzelle
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Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact
Optimum Shape Design for a Three Layer Interfacial Surfaces
Determining the Optimal Geometry for Producing Isotherms on a Boundary Surface
Powerplant Design and Performance Analysis of a Manned All-Electric Helicopter
Impact of Liquid-Hydrogen Fuel-Cell Electric Propulsion on Aircraft Configuration and Integration
Multistage Reliability-Based Design Optimization and Application to Aircraft Conceptual Design
Novel Propulsion Systems for Micro Aerial Vehicles