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Experimental study of the effects of flameholder geometry on emissions and performance of lean premixed combustorsEmissions of NOx, CO and unburned hydrocarbons (UHC) are reported for a lean premixed propane-air system at inlet conditions of 800K and 1 MPa using twelve flameholder designs. The flameholders tested represent six design concepts with two values of blockage for each concept. Data were obtained at reference velocities of 35 m/s, 25 m/s and 20 m/s at combustor stations 10 cm and 30 cm downstream of the flameholders. Flameholder pressure drop was found to be a principal determinant of emissions performance. Designs producing larger pressure drops also produced less NOx, CO and UHC emissions. The lean stability limit equivalence ratio was found to be approximately 0.35 for all designs. Flashback velocities (axial components in the flameholder passages) varied between 30 m/s and 40 m/s. A perforated plate flameholder was operated with a velocity as low as 23 m/s through the perforations at equivalence ratio 0.7 without producing flashback.
Document ID
19790035573
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roffe, G.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Venkataramani, K. S.
(General Applied Sciences Laboratories, Inc. Westbury, N.Y., United States)
Duerr, R. M.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AIAA PAPER 79-0187
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: New Orleans, LA
Start Date: January 15, 1979
End Date: January 17, 1979
Sponsors: Astronautics, American Institute of Aeronautics
Accession Number
79A19586
Distribution Limits
Public
Copyright
Other

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