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Calculations of condensation and chemistry in an aircraft contrailThe flow field, chemistry, and condensation nucleation behind a transport airplane are calculated in two regimes using two separate reacting flow codes: first the axisymmetric plume, then the three dimensional vortex wake. The included chemical kinetics equations follow the evolution of the NO(y) and SO(x) chemical families. In the plume regime, the chemistry is coupled with the binary homogeneous formation of sulfate condensation nuclei, where the calculated nucleation rates predict that copious quantities of H2SO4/H2O nuclei are produced in subnanometer sizes. These sulfate aerosols could play a major role in the subsequent condensation of water vapor and the formation of contrails under favorable atmospheric conditions.
Document ID
19950007367
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miake-Lye, Richard C.
(Aerodyne Products Corp. Billerica, MA, United States)
Brown, R. C.
(Aerodyne Products Corp. Billerica, MA, United States)
Anderson, M. R.
(Aerodyne Products Corp. Billerica, MA, United States)
Kolb, C. E.
(Aerodyne Products Corp. Billerica, MA, United States)
Date Acquired
August 17, 2013
Publication Date
May 24, 1994
Publication Information
Publication: DLR, Impact of Emissions From Aircraft and Spacecraft Upon the Atmosphere
Subject Category
Environment Pollution
Accession Number
95N13780
Funding Number(s)
CONTRACT_GRANT: DAAH01-93-C-R184
CONTRACT_GRANT: NAS1-19677
Distribution Limits
Public
Copyright
Other
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