Abstract
Linear instability sheet atomization (LISA) breakup model has been widely used for
modeling hollow-cone spray. However, the model was originally developed for inwardlyopening
pressure-swirl injectors by assuming toroidal ligament breakups. Therefore, LISA
model is not suitable for simulating outwardly opening injectors having string-like
structures at wide spray angles. Furthermore, the varying area and shape of the annular
nozzle exit makes the modeling difficult. In this study, a new spray modeling was proposed
for outwardly opening hollow-cone injector. The injection velocities are computed from the
given mas flow rate and injection pressure regardless of ambiguous nozzle exit geometries.
The modified Kelvin-Helmholtz and Rayleigh-Taylor (KH-RT) breakup model is used with
adjusted initial Sauter mean diameter (SMD) for modeling breakup of string-like liquid film
spray. Liquid spray injection was modeled using Lagrangian discrete parcel method within
the framework of commercial CFD software CONVERGE, and the detailed model was
implemented by user defined functions. It was found that the new model predicted the liquid
penetration length and local SMD accurately for various fuels and chamber conditions.
Original language | English (US) |
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Title of host publication | 54th AIAA Aerospace Sciences Meeting |
Publisher | American Institute of Aeronautics and Astronautics (AIAA) |
ISBN (Print) | 9781624103933 |
DOIs | |
State | Published - Jan 2 2016 |