Numerical study on flame acceleration and deflagration-to-detonation transition in a closed annular channel with a temperature-gradient jet flow
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0278997
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4413040794
