Abstract
A study is made of the thermal crisis of a vorticity source fl owing out into a rarefi ed space with the supersonic-tosubsonic transition in the compression shock followed by the deceleration of the subsonic fl ow in a submerged space. Consideration is given to a perfect gas with a constant heat capacity and with negligible thickness of the shock and thickness of the energy-release region. Dependences of the fl ow parameters on the parameter of mechanical-energy loss, the circulation, the coordinate of the energy-release region, and on the energy-supply parameter are studied.
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.
