Effect of Heat-Loss Boundary on Flame Acceleration and Deflagration-to-Detonation Transition in Narrow Channels

ABSTRACT

The entire process of deflagration-to-detonation transition (DDT) is studied through direct numerical simulations in narrow channels. Calculations with adiabatic and heat-loss boundaries are conducted to investigate the effect of heat loss to walls on flame acceleration and DDT. The numerical results show that heat loss reduces the flame acceleration rate and delays the occurrence of DDT. In the adiabatic channel, flame acceleration is caused mainly by viscosity friction with walls; ultra-fast flame in boundary layers plays a key role in the occurrence of DD. However, in the channel with heat loss the growth of the pressure pulse and the interaction of the leading shock with the boundary layers are weakened. Ultra-fast flame cannot be formed at the boundary layer in front of the flame surface and the occurrence of DDT is attributed to early burning in front of the flame.

KEYWORDS:

• Deflagration-to-detonation transition (DDT)
• Flame acceleration
• Heat loss
• Numerical simulation
• WENO

Funding

This work is supported by National Nature Science Foundation of China under grant numbers 11325209 and 11521062.

Additional information

Funding

This work is supported by National Nature Science Foundation of China under grant numbers 11325209 and 11521062.