TY - JOUR
T1 - Computational and experimental investigation of a swirl nozzle for viscous fluids
AU - Laurila, E.
AU - Koivisto, S.
AU - Kankkunen, A.
AU - Saari, K.
AU - Maakala, Viljami
AU - Jävinen, M.
AU - Vuorinen, V.
PY - 2020/7
Y1 - 2020/7
N2 - Highly viscous flow in a large-scale pressure-swirl atomizer is studied by (1) 3d scale-resolving large-eddy simulations and volume-of-fluid method, and (2) experiments based on laser-Doppler anemometry, imaging techniques and pressure measurements. Here, a low Reynolds number regime (600 ≤ Re ≤ 910) is investigated by varying the mass flow rate of the water-glycerol mixture. The aim of the study is to perform a comprehensive comparison between the simulations and experiments at a parameter range and nozzle geometry relevant for biomass based fuels. We report the inner-nozzle velocity profiles noting good agreement for mean velocities inside the swirl chamber between the simulations and the experiments. Consistent with the earlier work (Laurila et al., 2019), the simulations indicate the flow mode to be laminar with weak or non-existent gaseous core inside the swirl chamber. As revealed by both approaches, liquid film shapes after the nozzle discharge orifice are qualitatively similar, of hollow cone type, and highly unstable. Both approaches indicate linear scaling of the liquid film velocity with the inlet Reynolds number and discharge coefficients to be in the range 0.57–0.64. The experimentally measured mean opening angles are reported to be 45–62 ∘, while the numerical counterparts show reasonable correspondence with the experiments. The results demonstrate the predictive ability of the present numerical method in swirl injector analysis.
AB - Highly viscous flow in a large-scale pressure-swirl atomizer is studied by (1) 3d scale-resolving large-eddy simulations and volume-of-fluid method, and (2) experiments based on laser-Doppler anemometry, imaging techniques and pressure measurements. Here, a low Reynolds number regime (600 ≤ Re ≤ 910) is investigated by varying the mass flow rate of the water-glycerol mixture. The aim of the study is to perform a comprehensive comparison between the simulations and experiments at a parameter range and nozzle geometry relevant for biomass based fuels. We report the inner-nozzle velocity profiles noting good agreement for mean velocities inside the swirl chamber between the simulations and the experiments. Consistent with the earlier work (Laurila et al., 2019), the simulations indicate the flow mode to be laminar with weak or non-existent gaseous core inside the swirl chamber. As revealed by both approaches, liquid film shapes after the nozzle discharge orifice are qualitatively similar, of hollow cone type, and highly unstable. Both approaches indicate linear scaling of the liquid film velocity with the inlet Reynolds number and discharge coefficients to be in the range 0.57–0.64. The experimentally measured mean opening angles are reported to be 45–62 ∘, while the numerical counterparts show reasonable correspondence with the experiments. The results demonstrate the predictive ability of the present numerical method in swirl injector analysis.
KW - Pressure-swirl atomizer
KW - Water-glycerol mixture
KW - Large-eddy simulation
KW - Volume-of-fluid method
KW - Laser-Doppler anemometry
KW - High-speed imaging
KW - AIR-CORE
KW - INTERNAL FLOW
KW - NUMERICAL-SIMULATION
KW - PRIMARY ATOMIZATION
KW - SIMPLEX
KW - DYNAMICS
KW - ATOMIZER
UR - http://www.scopus.com/inward/record.url?scp=85089384670&partnerID=8YFLogxK
U2 - 10.1016/j.ijmultiphaseflow.2020.103278
DO - 10.1016/j.ijmultiphaseflow.2020.103278
M3 - Article
SN - 0301-9322
VL - 128
JO - International Journal of Multiphase Flow
JF - International Journal of Multiphase Flow
M1 - 103278
ER -