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Performance and durability of improved air-atomizing splash-cone fuel nozzlesAn improved design of air-atomizing fuel nozzles was determined from a study of four differently shaped splash-cone fuel nozzles after 56 hr of durability testing in a combustor segment. Test conditions included fuel-air ratios of 0.008 to 0.018, inlet-air total pressures of 41 to 203 N/cm, inlet-air temperatures of 477 to 811 K, and a reference velocity of 21.3 m/sec. Flat-tip fuel nozzles showed the least erosion damage and at a combustor operating condition of 700 K and 101 N/sq cm an oxides-of-nitrogen emission index of 12 and a smoke number of approximately 18 with a fuel-air ratio of 0.018. Emission indices for carbon monoxide and unburned hydrocarbons were 44 and 16, respectively, at simulated idle conditions of 477 K and 41 N/sq cm.
Document ID
19750004262
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ingebo, R. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Norgren, C. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-X-3156
E-8082
Report Number: NASA-TM-X-3156
Report Number: E-8082
Accession Number
75N12334
Funding Number(s)
PROJECT: RTOP 505-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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