O'Sullivan, MN and O'Sullivan, MN and Krasnodebski, JK and Krasnodebski, JK and Waitz, IA and Waitz, IA and Waitz, IA and Greitzer, EM and Greitzer, EM and Greitzer, EM and Tan, CS and Tan, CS and Tan, CS and Dawes, WN and Dawes, WN and Dawes, WN (1996) Computational study of viscous effects on lobed mixer flow features and performance. Journal of Propulsion and Power, 12. pp. 449-456. ISSN 0748-4658Full text not available from this repository.
This article describes a computational study of viscous effects on lobed mixer flowfields. The computations, which were carried out using a compressible, three-dimensional, unstructured-mesh Navier-Stokes solver, were aimed at assessing the impacts on mixer performance of inlet boundary-layer thickness and boundary-layer separation within the lobe. The geometries analyzed represent a class of lobed mixer configurations used in turbofan engines. Parameters investigated included lobe penetration angles from 22 to 45 deg, stream-to-stream velocity ratios from 0.5 to 1.0, and two inlet boundary-layer displacement thicknesses. The results show quantitatively the increasing influence of viscous effects as lobe penetration angle is increased. It is shown that the simple estimate of shed circulation given by Skebe et al. (Experimental Investigation of Three-Dimensional Forced Mixer Lobe Flow Field, AIAA Paper 88-3785, July, 1988) can be extended even to situations in which the flow is separated, provided an effective mixer exit angle and height are defined. An examination of different loss sources is also carried out to illustrate the relative contributions of mixing loss and of boundary-layer viscous effects in cases of practical interest.
|Divisions:||Div A > Turbomachinery|
|Depositing User:||Cron job|
|Date Deposited:||16 Jul 2015 13:31|
|Last Modified:||28 Aug 2015 04:43|