Derivation of pumpless reactant recirculation system based on analogy between fluid flow and electrical circuit for proton exchange membrane fuel cell

Author:

Uno Masatoshi1,Tanaka Koji1

Affiliation:

1. Japan Aerospace Exploration Agency; 2-1-1, Sengen Tsukuba, Ibaraki 305-8505 Japan

Publisher

Wiley

Subject

Electrical and Electronic Engineering

Reference29 articles.

1. Environmentally friendly power sources for aerospace applications;Rey;Journal of Power Sources,2008

2. Altitude testing of fuel cell systems for aircraft applications;Chang;SAE Transmission,2004

3. Efficiency and weight trade-off analysis of regenerative fuel cells as energy storage for aerospace applications;Barbir;Journal of Hydrogen Energy,2005

4. Fuel cells power aerospace vehicles;Oman;IEEE AESS System Magazine,2002

5. Development and demonstration flight of a fuel cell system for high-altitude balloons;Uno;Journal of Power Sources,2009

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