Effect of dilution air on the scalar flowfield at combustor sector exit
Author:
Affiliation:
1. General Electric Corporate R&D Center, Schenectady, New York 12301
2. General Electric Aircraft Engines, Cincinnati, Ohio 45215-6301
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23955
Reference16 articles.
1. Raman measurements at the exit of a combustor sector
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4. Study of Branched Turboprop Inlet Ducts Using a Multiple Block Grid Calculation Procedure
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