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Aerodynamic analysis of civil aeroengine exhaust systems using computational fluid dynamics

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dc.creator Otter, John J.
dc.creator Goulos, Ioannis
dc.creator MacManus, David G.
dc.creator Slaby, Michal
dc.date 2018-07-02T16:14:08Z
dc.date 2018-07-02T16:14:08Z
dc.date 2018-06-25
dc.date.accessioned 2022-05-25T16:36:46Z
dc.date.available 2022-05-25T16:36:46Z
dc.identifier Otter J, Goulos I, MacManus DGM, Slaby M, Aerodynamic analysis of civil aero-engine exhaust systems using computational fluid dynamics, Journal of Propulsion and Power, Vol. 34, No. 5 (2018), pp. 1152-1165
dc.identifier 0748-4658
dc.identifier http://dx.doi.org/10.2514/1.B36867
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/13299
dc.identifier 19781129
dc.identifier.uri http://localhost:8080/xmlui/handle/CUHPOERS/182158
dc.description As the specific thrust of civil aeroengines reduces, the aerodynamic performance of the exhaust system will become of paramount importance in the drive to reduce engine fuel burn. This paper presents an aerodynamic analysis of civil aeroengine exhaust systems through the use of Reynolds-averaged Navier–Stokes computational fluid dynamics. Two different numerical approaches are implemented, and the numerical predictions are compared to measured data from an experimental high-bypass-ratio separate-jet exhaust system. Over a fan nozzle pressure ratio range from 1.4 to 2.8, a comparison is drawn between values of the thrust coefficient calculated numerically and those obtained from experimental measurements. In addition, the effects of the freestream Mach number and extraction ratio on the aerodynamic behavior of the exhaust system are quantified and correlated to fundamental aerodynamic parameters.
dc.language en
dc.publisher AIAA
dc.rights Attribution-NonCommercial 4.0 International
dc.rights http://creativecommons.org/licenses/by-nc/4.0/
dc.subject Gas turbine
dc.subject Aerodynamics
dc.subject Computational fluid dynamics
dc.subject Exhaust
dc.subject Nozzles
dc.subject Turbofan
dc.title Aerodynamic analysis of civil aeroengine exhaust systems using computational fluid dynamics
dc.type Article


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