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Plume and wake dynamics, mixing, and chemistry behind an HSCT aircraftThe chemical evolution and mixing and vortical motion of a High Speed Civil Transport's engine exhausts must be analyzed in order to track the gas and its speciation as emissions are mixed to atmospheric scales. Attention is presently given to an analytic model of the wake dynamical processes which accounts for the roll-up of the trailing vorticity, its breakup due to the Crow instability, and the subsequent evolution and motion of the reconnected vorticity. The concentrated vorticity is noted to wrap up the buoyant exhaust and suppress its continued mixing and dilution. The species tracked encompass those which could be heterogeneously reactive on the surfaces of the condensed ice particles, and those capable of reacting with exhaust soot particle surfaces to form active contrail and/or cloud condensation nuclei.
Document ID
19910069449
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miake-Lye, R. C.
(Aerodyne Research, Inc. Billerica, MA, United States)
Martinez-Sanchez, M.
(Aerodyne Research, Inc. Billerica, MA, United States)
Brown, R. C.
(Aerodyne Research, Inc. Billerica, MA, United States)
Kolb, C. E.
(Aerodyne Research, Inc. Billerica, MA, United States)
Date Acquired
August 14, 2013
Publication Date
September 1, 1991
Subject Category
Environment Pollution
Report/Patent Number
AIAA PAPER 91-3158
Accession Number
91A54072
Funding Number(s)
CONTRACT_GRANT: NAS1-19161
Distribution Limits
Public
Copyright
Other

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