Kathy Simmons | University of Nottingham (original) (raw)
Uploads
Papers by Kathy Simmons
Volume 3: Turbo Expo 2005, Parts A and B, 2005
ABSTRACT
Computational Technologies for Fluid/Thermal/Structural/Chemical Systems With Industrial Applications, Volume 1, 2002
International Journal of Rotating Machinery
Computational Technologies for Fluid/Thermal/Structural/Chemical Systems With Industrial Applications, Volume 1, 2002
Journal of Engineering for Gas Turbines and Power, 2016
Volume 1: Advances in Aerospace Technology, 2015
Volume 5C: Heat Transfer, 2015
Volume 5C: Heat Transfer, 2015
International Journal of Rotating Machinery
Volume 5C: Heat Transfer, 2015
In aero engine bearing chambers oil is supplied for lubrication and cooling. Oil travels to the c... more In aero engine bearing chambers oil is supplied for lubrication and cooling. Oil travels to the chamber outer walls creating films that transport heat away from the hot surfaces. High speed oil droplets within the core flow impact onto surfaces and films during engine operation. To model this type of flow, there is a need to be able to account for the multiple impacting droplets and the resulting cooling film. Resolving the droplets explicitly is not yet computationally feasible for a full bearing chamber. A coupled Lagrangian-Eulerian methodology is therefore presented to describe the phenomenon at an affordable cost. The droplets are assumed to be point particles and coupled with the Eulerian phase upon impact. Test cases reported here compare well with published literature.
This paper presents a low cost Computational Fluid Dynamics (CFD) technique for the modelling of ... more This paper presents a low cost Computational Fluid Dynamics (CFD) technique for the modelling of droplet to film impact with heat transfer. In this approach the liquid and gas continua are modelled using an enhanced Volume of Fluid (VoF) technique while the droplets are tracked using a Lagrangian framework and are coupled to the Eulerian phases using source terms. The eventual target application is an aeroengine bearing chamber in which oil is found as droplets, shed from the bearings, separated from wall surfaces at obstacles or simply re-entrained, and as a continuum oil film coating the chamber outer walls which it also cools. A generic algorithm has therefore been developed to track the gas-liquid interface and determine the occurrence and scenario and outcome of impact between the Lagrangian and Eulerian representations of the liquid, based on correlations. The proposed technique has been tested for the case of a spray nozzle and satisfactorily evaluated against published exper...
Computational Technologies for Fluid/Thermal/Structural/Chemical Systems With Industrial Applications, Volume 1, 2002
Volume 1: Advances in Aerospace Technology, 2014
Volume 5C: Heat Transfer, 2014
Volume 5C: Heat Transfer, 2014
Volume 4: Turbo Expo 2004, 2004
Volume 3: Turbo Expo 2005, Parts A and B, 2005
ABSTRACT
Computational Technologies for Fluid/Thermal/Structural/Chemical Systems With Industrial Applications, Volume 1, 2002
International Journal of Rotating Machinery
Computational Technologies for Fluid/Thermal/Structural/Chemical Systems With Industrial Applications, Volume 1, 2002
Journal of Engineering for Gas Turbines and Power, 2016
Volume 1: Advances in Aerospace Technology, 2015
Volume 5C: Heat Transfer, 2015
Volume 5C: Heat Transfer, 2015
International Journal of Rotating Machinery
Volume 5C: Heat Transfer, 2015
In aero engine bearing chambers oil is supplied for lubrication and cooling. Oil travels to the c... more In aero engine bearing chambers oil is supplied for lubrication and cooling. Oil travels to the chamber outer walls creating films that transport heat away from the hot surfaces. High speed oil droplets within the core flow impact onto surfaces and films during engine operation. To model this type of flow, there is a need to be able to account for the multiple impacting droplets and the resulting cooling film. Resolving the droplets explicitly is not yet computationally feasible for a full bearing chamber. A coupled Lagrangian-Eulerian methodology is therefore presented to describe the phenomenon at an affordable cost. The droplets are assumed to be point particles and coupled with the Eulerian phase upon impact. Test cases reported here compare well with published literature.
This paper presents a low cost Computational Fluid Dynamics (CFD) technique for the modelling of ... more This paper presents a low cost Computational Fluid Dynamics (CFD) technique for the modelling of droplet to film impact with heat transfer. In this approach the liquid and gas continua are modelled using an enhanced Volume of Fluid (VoF) technique while the droplets are tracked using a Lagrangian framework and are coupled to the Eulerian phases using source terms. The eventual target application is an aeroengine bearing chamber in which oil is found as droplets, shed from the bearings, separated from wall surfaces at obstacles or simply re-entrained, and as a continuum oil film coating the chamber outer walls which it also cools. A generic algorithm has therefore been developed to track the gas-liquid interface and determine the occurrence and scenario and outcome of impact between the Lagrangian and Eulerian representations of the liquid, based on correlations. The proposed technique has been tested for the case of a spray nozzle and satisfactorily evaluated against published exper...
Computational Technologies for Fluid/Thermal/Structural/Chemical Systems With Industrial Applications, Volume 1, 2002
Volume 1: Advances in Aerospace Technology, 2014
Volume 5C: Heat Transfer, 2014
Volume 5C: Heat Transfer, 2014
Volume 4: Turbo Expo 2004, 2004