Abstract
The geometric parameters of a separation zone originating during interaction between a supersonic stream and a transverse gas jet are considered. An approximate similarity law, which is verified by experimental results, is formulated for the presence of a high-intensity jet. The case when the separation point reaches the leading edge of the body or is fixed at a point of a sharp break in the body contour is considered specially.
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.
