Abstract
The detonation combustion of a supersonic flow of propane-air mixture, initiated by a pulsed discharge of a magnetoplasma compressor, is obtained in experiment. A backward wave of supersonic combustion propagating with a velocity of 450 m/s against the flow is observed.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: 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.