In
this article, premixed methane–air flame propagation
in a confined vessel at low initial temperature was simulated using
a multistep chemical reaction mechanism. The confined vessel was a
cylinder with aspect ratio of 3 with asymmetrical position of the
ignition source near the side cover. The equivalence ratio and the
initial temperature of the premixed unburned combustible gas were
1.0 and 150 K, respectively. The overall evolution of the flame and
the flame dynamics were obtained, respectively. Through the entire
flow field variation, vortex movement, and pressure wave propagation
characteristics during the whole process of combustion, the flame
propagation mechanism of methane combustion at low initial temperature
was established finally. Results indicate that five stages are divided
during the methane combustion in a confined vessel: spherical flame
propagation, “fingertip” shaped flame propagation, flame
“skirt edge” contacts the side wall, “crescent”
flame propagation, and typical “tulip” flame propagation.
In the process of flame propagation, the reverse of the flame front
and formation of the “tulip” flame can be immediately
contributed to the interaction of the flame front, flame induced reverse
flow, and vortex motion. However, the pressure wave propagation back
and forth along the flame propagation direction has no obvious effect
on the formation of tulip flame. When the distorted tulip flame is
formed, vortex motion is not observed. The formation of the distorted
tulip flame is caused by the superposition of the secondary pressure
wave formed by the contact of the flame with side wall. However, because
of the low intensity of pressure wave, RT instability is weak, and
the distortion of flame front is not obvious. Flame propagation velocity
and pressure wave are interacted with each other. In the process of
combustion, the variation of flame propagation velocity and pressure
rise rate show almost the same phase. The increase in flame propagation
velocity directly leads to the increase in pressure rise rate, whereas
the pressure wave propagation back and forth in the confined vessel
leads to the oscillation of propagation velocity.