dynamics of aircraft exhaust plumes in the jet-regime

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Annales Geophysicae ISSN: 0992-7689 (printed version) ISSN: 1432-0576 (electronic version) Abstract Volume 12 Issue 10/11 (1994) pp 911-919 Dynamics of aircraft exhaust plumes in the jet-regime B. Kärcher, P. Fabian Lehrstuhl für Bioklimatologie und Immissionsforschung, Universität München, Hohenbachernstr. 22, D-85354 Freising, Germany Received: 22 September 1993/Revised: 24 January 1994/Accepted: 28 February 1994 Abstract. A computational model describing the two-dimensional, turbulent mixing of a single jet of exhaust gas from aircraft engines with the ambient atmosphere is presented. The underlying assumptions and governing equations are examined and supplemented by a discussion of analytical solutions. As an application, the jet dynamics of a B747-400 aircraft engine in cruise and its dependence on key parameters is investigated in detail. The computer code for this dynamical model is computationally fast and can easily be coupled to complex chemical and microphysical models in order to perform comprehensive studies of atmospheric effects from aircraft exhaust emissions in the jet regime. Article not available online Last change: October 3, 1997 [email protected] © Springer Berlin Heidelberg 1994

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Annales Geophysicae

ISSN: 0992-7689 (printed version)ISSN: 1432-0576 (electronic version)

Abstract Volume 12 Issue 10/11 (1994) pp 911-919

Dynamics of aircraft exhaust plumes in the jet-regime

B. Kärcher, P. Fabian

Lehrstuhl für Bioklimatologie und Immissionsforschung, Universität München, Hohenbachernstr. 22, D-85354 Freising, Germany

Received: 22 September 1993/Revised: 24 January 1994/Accepted: 28 February 1994

Abstract. A computational model describing the two-dimensional, turbulent mixing of a single jet of exhaust gas from aircraftengines with the ambient atmosphere is presented. The underlying assumptions and governing equations are examined andsupplemented by a discussion of analytical solutions. As an application, the jet dynamics of a B747-400 aircraft engine in cruiseand its dependence on key parameters is investigated in detail. The computer code for this dynamical model is computationallyfast and can easily be coupled to complex chemical and microphysical models in order to perform comprehensive studies ofatmospheric effects from aircraft exhaust emissions in the jet regime.

Article not available online

Last change: October 3, [email protected]© Springer Berlin Heidelberg 1994