TY - GEN
T1 - Numerical Analysis of Aerial Firefighting Using Grid–Particle Coupling Method
AU - Tsujimura, Hiroki
AU - Kubota, Kenichi
AU - Sato, Tetsuya
N1 - Funding Information:
Hiroki Tsujimura was financially supported by the Research Fellowships of Japan Society for the Promotion of Science (JSPS) for Young Scientists under grant number 20J21930. JAXA Supercomputer System Generation 3 (JSS3) was used in obtaining the results. The authors would like to thank Dr. Takeshi Ito and Dr. Hiroyuki Kato of Japan Aerospace Exploration Agency, Mr. Shinji Tagawa and Mr. Yushi Goda of ShinMaywa Industries, Ltd., and Mr. Eiichi Negishi of Japan Aircraft Development Corporation for providing the wind tunnel test results. The authors would also like to thank Dr. Shigeru Kuchiishi of Japan Aerospace Exploration Agency for helpful discussions.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - Aerial firefighting is a common measure to extinguish forest fires and is expected to be helpful in managing urban disasters. Numerical analysis is an effective approach in the development of a firefighting aircraft because numerous tests with different conditions including aircraft speed, water amount, and fluid properties can be conducted at low cost. A combination of the Volume of Fluid method and the Discrete Droplet Model is widely used, but the method requires theoretical or empirical models that affect the calculation result. In this paper, as an alternative approach, the grid–particle coupling method is applied to numerical analyses of water spray from a firefighting aircraft. In the method, gas and liquid phases are calculated by grid and particle methods respectively, and they are coupled using the Aerodynamic Force Model developed by the authors. Results show that water spray behavior such as column breakup and surface breakup, and features of the waterfall distribution on the wind tunnel floor, can be qualitatively captured. Introducing a sub-grid scale aerodynamic model was effective in enhancing atomization and obtaining a successful result.
AB - Aerial firefighting is a common measure to extinguish forest fires and is expected to be helpful in managing urban disasters. Numerical analysis is an effective approach in the development of a firefighting aircraft because numerous tests with different conditions including aircraft speed, water amount, and fluid properties can be conducted at low cost. A combination of the Volume of Fluid method and the Discrete Droplet Model is widely used, but the method requires theoretical or empirical models that affect the calculation result. In this paper, as an alternative approach, the grid–particle coupling method is applied to numerical analyses of water spray from a firefighting aircraft. In the method, gas and liquid phases are calculated by grid and particle methods respectively, and they are coupled using the Aerodynamic Force Model developed by the authors. Results show that water spray behavior such as column breakup and surface breakup, and features of the waterfall distribution on the wind tunnel floor, can be qualitatively captured. Introducing a sub-grid scale aerodynamic model was effective in enhancing atomization and obtaining a successful result.
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U2 - 10.2514/6.2022-0450
DO - 10.2514/6.2022-0450
M3 - Conference contribution
AN - SCOPUS:85122911595
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -