Integrated computations of an entire jet engine

Gorazd Medic, Donghyun You, Georgi Kalitzin, Marcus Herrmann, Frank Ham, Heinz Pitsch, Edwin Van Der Weide, Juan Alonso

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Scopus citations

Abstract

In this paper, we present a framework that we have developed for integrated computations of an entire jet engine. It is based on a software environment, CHIMPS, that allows a simulation of multi-component effects by executing multiple solvers simultaneously. Each of these solvers computes a portion of a given flow domain and exchanges flow data at the interfaces with its peer solvers. We demonstrated this approach in a simulation of a 20 degree sector of the entire gas turbine jet engine, encompassing the fan, low and high pressure compressor, combustor, high and low pressure turbine and the exit nozzle. We will show that such a simulation can deliver important insight into the physics of interaction between different engine components, within a reasonable turnover time, which is necessary for it to be useful in the design process of an engine.

Original languageEnglish (US)
Title of host publicationProceedings of the ASME Turbo Expo 2007 - Power for Land, Sea, and Air
Pages1841-1847
Number of pages7
DOIs
StatePublished - Sep 25 2007
Event2007 ASME Turbo Expo - Montreal, Que., Canada
Duration: May 14 2007May 17 2007

Publication series

NameProceedings of the ASME Turbo Expo
Volume6 PART B

Other

Other2007 ASME Turbo Expo
CountryCanada
CityMontreal, Que.
Period5/14/075/17/07

ASJC Scopus subject areas

  • Engineering(all)

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  • Cite this

    Medic, G., You, D., Kalitzin, G., Herrmann, M., Ham, F., Pitsch, H., Van Der Weide, E., & Alonso, J. (2007). Integrated computations of an entire jet engine. In Proceedings of the ASME Turbo Expo 2007 - Power for Land, Sea, and Air (pp. 1841-1847). (Proceedings of the ASME Turbo Expo; Vol. 6 PART B). https://doi.org/10.1115/GT2007-27094