Affiliation:
1. G.E. Aircraft Engines, Cincinnati, OH
Abstract
The concept of the Swirl Number and its effect on recirculation is reviewed and problems with it are identified. Swirl generation through the use of radial inlet swirl vanes is then studied. The effect of vane and swirl cup design on recirculation is then evaluated using finite element computer modeling and verified using tufting tests. Vane geometry, combustor dome geometry, co- vs. counter-rotation and mass flow effects are all evaluated. It is shown that co- and counter-rotation generate very similar flow fields and recirculated mass flows. An approach for calculating swirl numbers in multiple swirler designs is proposed.
Publisher
American Society of Mechanical Engineers
Cited by
4 articles.
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1. Oxygen transfer characteristics of swirl and non-swirl plunging jets;ISH Journal of Hydraulic Engineering;2022-12-12
2. Design and CFD simulation of triple swirler in jet engine;2ND INTERNATIONAL CONFERENCE ON ADVANCED RESEARCH IN MECHANICAL ENGINEERING (2ND ICARME – 21);2022
3. Evaluation of Fuel Distribution in a Gas-Turbine Premixer: Influence of Swirl;Journal of Propulsion and Power;1999-09
4. Fuel Nozzle Aerodynamic Design Using CFD Analysis;Journal of Engineering for Gas Turbines and Power;1997-07-01