posted on 2018-04-17, 13:24authored byJonathan F. Carrotte
An experimental investigation has been carried out into the mixing of a row of jets
injected into a confined cross-flow. Measurements were made on a fully annular test facility,
the geometry of the rig simulating that found in the dilution zone of a gas turbine combustion
chamber. A small temperature difference of 44°C between the cross-flow and dilution fluid
allowed the mixing characteristics to be assessed, with hot jets being injected into a relatively
cold cross-flow at a jet to cross-flow momentum flux ratio of 4.0. The investigation
concentrated on differences in the mixing of individual dilution jets, as indicated by the
regularity of the temperature patterns around the cross-flow annulus. Despite the uniform
conditions approaching the dilution holes there were significant differences in the temperature
patterns produced by the dilution jets around the annulus. [Continues.]
Funding
Great Britain, Royal Aerospace Establishment (Pyestock), contract no. D/ERl/9/4/2170/113/RAE(P).
History
School
Aeronautical, Automotive, Chemical and Materials Engineering
This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/
Publication date
1990
Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy at Loughborough University.