Mechanism of flame acceleration and detonation transition from the interaction of a supersonic turbulent flame with an obstruction
Willstrong Rakotoarison, Brian Maxwell, Andrzej Pekalski, Matei I., Radulescu

TL;DR
This study investigates how turbulent flames accelerate and transition to detonation when interacting with obstacles, revealing that shock reflection enhances turbulent burning rates leading to detonation, primarily driven by increased turbulent combustion rather than auto-ignition.
Contribution
It provides experimental and numerical insights into the mechanism of flame acceleration and detonation transition caused by shock-flame interactions with obstacles.
Findings
Shock reflection enhances turbulent burning rate.
Flame velocity approaches the speed of sound, amplifying shocks.
Detonation occurs in regions with non-planar internal shocks.
Abstract
The present paper seeks to determine the mechanism of flame acceleration and transition to detonation when a turbulent flame preceded by a shock interacts with a single obstruction in its path, taken as a cylindrical obstacle or a wall in the present study. The problem is addressed experimentally in a mixture of propane-oxygen at sub-atmospheric conditions. The turbulent flame was generated by passing a detonation wave through a perforated plate, yielding flames with turbulent burning velocities 10 to 20 larger than the laminar values and incident shock Mach numbers ranging between 2 and 2.5. Time resolved schlieren videos recorded at approximately 100 kHz and numerical reconstruction of the flow field permitted to determine the mechanism of flame acceleration and transition to detonation. It was found to be the enhancement of the turbulent burning rate of the flame through its…
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Taxonomy
TopicsCombustion and Detonation Processes · Combustion and flame dynamics · Computational Fluid Dynamics and Aerodynamics
