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Parametric Design of Injectors for LDI-3 Combustors

Authors :
Hukam Mongia
Kumud Ajmani
Phil Lee
Source :
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Publication Year :
2015
Publisher :
American Institute of Aeronautics and Astronautics, 2015.

Abstract

Application of a partially calibrated National Combustion Code (NCC) for providing guidance in the design of the 3rd generation of the Lean-Direct Injection (LDI) multi-element combustion configuration (LDI-3) is summarized. NCC was used to perform non-reacting and two-phase reacting flow computations on several LDI-3 injector configurations in a single-element and a five-element injector array. All computations were performed with a consistent approach for mesh-generation, turbulence, spray simulations, ignition and chemical kinetics-modeling. Both qualitative and quantitative assessment of the computed flowfield characteristics of the several design options led to selection of an optimal injector LDI- 3 design that met all the requirements including effective area, aerodynamics and fuel-air mixing criteria. Computed LDI-3 emissions (namely, NOx, CO and UHC) will be compared with the prior generation LDI- 2 combustor experimental data at relevant engine cycle conditions.

Details

Database :
OpenAIRE
Journal :
51st AIAA/SAE/ASEE Joint Propulsion Conference
Accession number :
edsair.doi...........ca708b95304368080cdff2a8f50ea360