Abstract

It has been established from a theoretical and experimental analysis of aerodynamic characteristics of acoustically modulated gas jets that, in the subcritical flow regime, acoustic vibrations affect the turbulent jet divergence at the exit from the jet–acoustic generator. It has been proved that the acoustic action on the core of a turbulent jet results in the hysteresis in the jet–acoustic system. This effect has been substantiated theoretically and the influence on the density of the reflecting surface on the hysteresis loop width has been confirmed experimentally.

Full Text
Paper version not known

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 call

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.