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Gaseous Emissions Results from a Three-Cup Flametube Test of a Third-Generation Swirl-Venturi Lean Direct Injection Combustion ConceptThis paper summarizes the development of lean direct injection (LDI) combustor technology at, or in collaboration with, the NASA Glenn Research Center. These configurations differ mainly in fuel-air mixing strategy. The paper reviews the NOx performance and operability characteristics of multiple LDI configurations tested at NASA Glenn.
Document ID
20170008735
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Tacina, Kathleen M. (NASA Glenn Research Center Cleveland, OH United States)
Podboy, Derek P. (NASA Glenn Research Center Cleveland, OH United States)
Lee, Phil (Woodard, Inc. Zeeland, MI, United States)
Dam, Bidhan (Woodard, Inc. Zeeland, MI, United States)
Date Acquired
September 11, 2017
Publication Date
September 3, 2017
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN44327
Meeting Information
Meeting: International Society of Air Breathing Engines (ISABE) Conference 2017
Location: Manchester, England
Country: United Kingdom
Start Date: September 3, 2017
End Date: September 8, 2017
Sponsors: International Society for Air Breathing Engines (ISABE)
Funding Number(s)
WBS: WBS 081876.02.03.04.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
emissions
combustor
NOx

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