Abstract
It was shown experimentally for the first time that, when an axisymmetric nozzle of special shape is placed in a tube, the shocktodetonation transition in a stoichiometric natural gas-air mixture occurs under normal conditions at a shock wave (SW) velocity at the nozzle inlet exceeding 1150 ± 30 m/s, which corre� sponds approximately to a Mach number of 3.3. This finding is important for the development of newgen� eration burners using pulsed detonative (PD) combus� tion of natural gas, as well as for a better understanding of the dynamics of accidental gas explosions in mine
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
