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Fuel Reformer Nozzle DevelopmentThe fellowship work this summer will be in support of the development of a fuel mixer for a liquid fuel reformer that is upstream of a fuel cell. Tasks for the summer shall consist of design of a fuel mixer, setup of the laser diagnostics for determining the degree of fuel mixing, and testing of the fuel mixer. The fuel mixer shall be a venturi section with fuel injected at or near the throat, and an air swirler upstream of the venturi. Data to determine the performance of the mixer shall be taken using a Phase Doppler Particle Analyzer (PDPA).
Document ID
20040151770
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Lai, Ming-Chia D. (Wayne State Univ. Detroit, MI, United States)
Date Acquired
August 22, 2013
Publication Date
January 1, 2003
Publication Information
Publication: NASA-OAI Collaborative Aerospace Research and Fellowship Program
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle20040151764Collected WorksNASA-OAI Collaborative Aerospace Research and Fellowship Program
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