TY - GEN
T1 - Evaporation of Three-Dimensional Wavy Liquid Film Entrained by Turbulent Gas Flow
AU - Inoue, Chihiro
AU - Maeda, Ikkan
AU - Fujii, Go
AU - Daimon, Yu
N1 - Funding Information:
This study was supported by JSPS KAKENHI, JP21H01251.
Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2021
Y1 - 2021
N2 - For predicting the length of coolant liquid film extending inside a combustion chamber of bipropellant thruster, we develop an original theoretical model, newly incorporating the three-dimensional film dynamics and evaporation. The large velocity difference between the slow liquid film and fast combustion gas initially induces Kelvin-Helmholtz instability as roll wave, followed by transverse Rayleigh-Taylor instability as ripple wave. Superposing the two types of instabilities produce conical cusps as the origin of ligaments on the liquid film, ejecting entraining droplets, which reduce net coolant film flow rate. The conical cusps simultaneously enlarges the heat transfer area of the film subjected to the hot combustion gas. Implementing both effects of the entrainment and wet area expansion into the heat balance between the latent heat of the film and convective heat transfer from the combustion gas, we successfully predict the film coolant length of corresponding combustion test results, presenting that the film length shortens according to the increment of combustion pressure.
AB - For predicting the length of coolant liquid film extending inside a combustion chamber of bipropellant thruster, we develop an original theoretical model, newly incorporating the three-dimensional film dynamics and evaporation. The large velocity difference between the slow liquid film and fast combustion gas initially induces Kelvin-Helmholtz instability as roll wave, followed by transverse Rayleigh-Taylor instability as ripple wave. Superposing the two types of instabilities produce conical cusps as the origin of ligaments on the liquid film, ejecting entraining droplets, which reduce net coolant film flow rate. The conical cusps simultaneously enlarges the heat transfer area of the film subjected to the hot combustion gas. Implementing both effects of the entrainment and wet area expansion into the heat balance between the latent heat of the film and convective heat transfer from the combustion gas, we successfully predict the film coolant length of corresponding combustion test results, presenting that the film length shortens according to the increment of combustion pressure.
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U2 - 10.2514/6.2021-3706
DO - 10.2514/6.2021-3706
M3 - Conference contribution
AN - SCOPUS:85126786364
SN - 9781624106118
T3 - AIAA Propulsion and Energy Forum, 2021
BT - AIAA Propulsion and Energy Forum, 2021
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy Forum, 2021
Y2 - 9 August 2021 through 11 August 2021
ER -