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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 1MPa 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
19780018204
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roffe, G.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Venkataramani, K. S.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-135424
GASL-TR-249
Report Number: NASA-CR-135424
Report Number: GASL-TR-249
Accession Number
78N26147
Funding Number(s)
CONTRACT_GRANT: NAS3-20603
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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