«Detailed Program

ID 367

Eulerian / Lagrangian Simulation of Aerated-Liquid Injection into Subsonic and Supersonic Crossflows

Joseph Talbot
North Carolina State University
United States

Anupam Kulkarni
North Carolina State University
United States

Jack Edwards
North Carolina State University
United States

Kuo-Cheng Lin
Taitech, Inc
United States

Brett Bornhoft
U.S. Air Force Research Laboratory
United States

 

Abstract:

Aerated-liquid or ‘barbotage’ atomization initiates primary breakup by injecting a small amount of gas into a co-flowing liquid and then expanding the mixture through a small-orifice nozzle. At high gas-to-liquid mass ratios, the result is a highly-turbulent two-phase flow that can be characterized as having a core-annular structure. The core is populated by fine-scale droplets, shed from the annular liquid film by aerodynamic forces. The injection of the two-phase flow into a crossflow environment results in the breakup of the annular liquid sheet followed possibly by secondary droplet breakup mechanisms. An Eulerian homogeneous mixture model, evolved as a large-eddy simulation, will be combined with a parallel Lagrangian droplet-tracking algorithm to simulate the evolution of the initially dense spray. Factors included in the droplet-tracking model include dense-spray effects on drag forces, secondary droplet breakup mechanisms, and separate initial droplet size distributions for core and annular regions. Results will be obtained for two cases: one involving ‘out-in’ aerated liquid injection into a Mach 0.3 subsonic crossflow and the other involving aerated-liquid injection into a Mach 2.0 supersonic crossflow. Predictions will be compared with confocal X-ray fluorescence measurements for the subsonic crossflow experiments and with phase Doppler particle anemometry and laser-sheet illumination data for the supersonic crossflow experiments.