TY - GEN
T1 - Numerical investigation of a submerged water jet impinging at various angles on ground
AU - Zhang, Xiang
AU - Agarwal, Ramesh K.
AU - Gao, Han
AU - Zhou, Ling
N1 - Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - This paper studies the impingement on ground of a submerged round water jet of diameter 0.02 m at angles of 15, 30, 45, 60, 75 and 90 degree by numerical simulation. Reynolds number at jet exit is 23,400 and the height between the exit of jet pipe and impingement plane is 0.06m. For numerical simulation, Reynolds-Averaged Navier-Stokes (RANS) equations are solved with realizable k-ε and Wray-Agarwal (WA) turbulence models using the commercial CFD solver ANSYS FLUENT. Pre-and post-processing are done by ICEM-CFD, CFD-POST and Origin Lab. Results from numerical simulations are compared with the experimental data and show that both turbulence models obtain results in reasonably good agreement with the experimental data, while WA model shows some improvement over the realizable k-ε model. Differences between the numerical and experimental results are analyzed.
AB - This paper studies the impingement on ground of a submerged round water jet of diameter 0.02 m at angles of 15, 30, 45, 60, 75 and 90 degree by numerical simulation. Reynolds number at jet exit is 23,400 and the height between the exit of jet pipe and impingement plane is 0.06m. For numerical simulation, Reynolds-Averaged Navier-Stokes (RANS) equations are solved with realizable k-ε and Wray-Agarwal (WA) turbulence models using the commercial CFD solver ANSYS FLUENT. Pre-and post-processing are done by ICEM-CFD, CFD-POST and Origin Lab. Results from numerical simulations are compared with the experimental data and show that both turbulence models obtain results in reasonably good agreement with the experimental data, while WA model shows some improvement over the realizable k-ε model. Differences between the numerical and experimental results are analyzed.
UR - http://www.scopus.com/inward/record.url?scp=85092400247&partnerID=8YFLogxK
U2 - 10.2514/6.2020-2038
DO - 10.2514/6.2020-2038
M3 - Conference contribution
AN - SCOPUS:85092400247
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -