Experimental Investigation of a Multiplex Fuel Injector Module with Discrete Jet Swirlers for Low Emission Combustors
Author:
Affiliation:
1. NASA Glenn Research Center
2. Goodrich
3. QSS Group Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-135
Reference16 articles.
1. Low NO(x) potential of gas turbine engines
2. Experimental Investigation of a Multiplex Fuel Injector Module for Low Emission Combustors
3. SAE ARP1533-1996, "Procedure for the Calculation of Gaseous Emissions from Aircraft Turbine Engines."
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