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Aircraft Particle Emissions eXperiment (APEX)APEX systematically investigated the gas-phase and particle emissions from a CFM56-2C1 engine on NASA's DC-8 aircraft as functions of engine power, fuel composition, and exhaust plumage. Emissions parameters were measured at 11 engine power, settings, ranging from idle to maximum thrust, in samples collected at 1, 10, and 30 m downstream of the exhaust plane as the aircraft burned three fuels to stress relevant chemistry. Gas-phase emission indices measured at 1 m were in good agreement with the ICAO data and predictions provided by GEAE empirical modeling tools. Soot particles emitted by the engine exhibited a log-normal size distribution peaked between 15 and 40 nm, depending on engine power. Samples collected 30 m downstream of the engine exhaust plane exhibited a prominent nucleation mode.
Document ID
20060046626
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Wey, C. C.
(Army Research Lab. Cleveland, OH, United States)
Anderson, B. E.
(NASA Langley Research Center Hampton, VA, United States)
Hudgins, C.
(NASA Langley Research Center Hampton, VA, United States)
Wey, C.
(QSS Group, Inc. Cleveland, OH, United States)
Li-Jones, X.
(Toledo Univ. OH, United States)
Winstead, E.
(G and A Technical Software, Inc. Newport News, VA, United States)
Thornhill, L. K.
(Science Applications International Corp. Hampton, VA, United States)
Lobo, P.
(Missouri Univ. Rolla, MO, United States)
Hagen, D.
(Missouri Univ. Rolla, MO, United States)
Whitefield, P.
(Missouri Univ. Rolla, MO, United States)
Date Acquired
August 23, 2013
Publication Date
September 1, 2006
Subject Category
Environment Pollution
Report/Patent Number
E-15660
NASA/TM-2006-214382
ARL-TR-3903
Funding Number(s)
WBS: WBS 754-02-07-03-06-01
Distribution Limits
Public
Copyright
Public Use Permitted.
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