Open AccessInfluence of the relative momentum flux ratio on the mixing of hydrogen jets in an M=4 crossflow
Author(s) -
Н. Н. Федорова,
M. A. Goldfeld,
S. A. Valger
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1677/1/012039
Subject(s) - mechanics , mach number , turbulence , jet (fluid) , momentum (technical analysis) , reynolds number , physics , mixing (physics) , overall pressure ratio , computational fluid dynamics , flow (mathematics) , flux (metallurgy) , thermodynamics , wind tunnel , materials science , gas compressor , finance , quantum mechanics , economics , metallurgy
The paper presents the results of numerical simulation of the 3D flows in a plane channel with the abrupt expansion. Sonic hydrogen jets are supplied from two circle orifices located opposite each other on the channel walls before the backward-facing step. The numerical simulations are carried out under the conditions of experiments performed at the hot-shot wind tunnel IT-302M ITAM SB RAS for the following flow parameters: Mach number at the entrance of the channel M = 3.84, the total temperature T 0 = 1715 K, and the total pressure P 0 = 6.5 MPa. Calculations were performed with a change in the jet supply pressure from 0.4 to 3.6 MPa, which ensures the variation in the jet-to-crossflow momentum flux ratio in the range of J = 0.7 ÷ 6. Mathematical modeling was performed in ANSYS Fluent based on the Reynolds-Averaged Navier-Stokes equations supplemented by the k-ω SST turbulence model. A comparison of the calculated and experimental data on the flow structure, as well as the static pressure distributions on the walls, indicates a satisfactory agreement. The calculated results made it possible to obtain a clearer understanding of the 3D flow structure in the channel and reveal the influence of the injection pressure on the level of mixing.