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<!DOCTYPE article SYSTEM "http://www.atmos-chem-phys-discuss.net/inc/acpd/copernicus.dtd">
<article language="en">
	<journal>
		<journal_title>Atmospheric Chemistry and Physics Discussions</journal_title>
		<journal_url>www.atmos-chem-phys-discuss.net</journal_url>
		<issn>1680-7367</issn>
		<eissn>1680-7375</eissn>
		<volume_number>2</volume_number>
		<issue_number>6</issue_number>
		<publication_year>2002</publication_year>
	</journal>
	<doi>10.5194/acpd-2-2045-2002</doi>
	<article_url>http://www.atmos-chem-phys-discuss.net/2/2045/2002/</article_url>
	<abstract_html>http://www.atmos-chem-phys-discuss.net/2/2045/2002/acpd-2-2045-2002.html</abstract_html>
	<fulltext_pdf>http://www.atmos-chem-phys-discuss.net/2/2045/2002/acpd-2-2045-2002.pdf</fulltext_pdf>
	<start_page>2045</start_page>
	<end_page>2074</end_page>
	<publication_date>2002-11-13</publication_date>
	<article_title content_type="html">Emission of ions and charged soot particles by aircraft engines</article_title>
	<authors>
		<author numeration="1" affiliations="1">
			<name>A. Sorokin</name>
		</author>
		<author numeration="2" affiliations="2">
			<name>X. Vancassel</name>
		</author>
		<author numeration="3" affiliations="2">
			<name>P. Mirabel</name>
		</author>
	</authors>
	<affiliations>
		<affiliation numeration="1" content_type="html">Central Institute of Aviation Motors, 2 Aviamotornaya str., 111116, Moscow, Russia</affiliation>
		<affiliation numeration="2" content_type="html">Centre de Géochimie de la Surface, CNRS and Université Louis Pasteur 1, rue Blessig, F-67084 Strasbourg France</affiliation>
	</affiliations>
	<abstract content_type="html">In this article, a model which examines the formation and evolution of chemiions  in an
      aircraft engine is proposed. This model which includes chemiionisation, electron thermo-emission,
      electron attachment to soot particles and to neutral molecules, electron-ion and ion-ion recombination,
      ion-soot interaction, allows the determination of the ion concentration at
      the exit of the combustor and at the nozzle exit of the engine. It also allows the determination
      of the charge of the soot particles. A comparison of the model results with the available
      ground-based experimental data obtained on the ATTAS research aircraft engines during the
      SULFUR experiments (Schumann, 2002) shows an excellent agreement.</abstract>
	<references>
	</references>
</article>

