Abstract
The three-dimensional compressible Navier-Stokes equations are numerically solved to study the transitional structure and the resultant acoustic emission in a supersonic round jet at high convective Mach numbers. Numerical results for the convective Mach number Mc = 1.00 (Mj=2.0) and Rer0=2000 based on the jet nozzle radius r0 are presented. Four different cases were investigated. These cases are the jet flow forced by random disturbances with various dominant wave length λmax. Numerical results suggest that the random inlet disturbance with short wave length affects transition largely compared with long wavelength. However, in the case where the potential core length is the same, the effect of dominant wave length of inlet random disturbance on transition structures and sound fields is small in the super sonic round jet.
Sign-in/Register to access full text options 
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 callMore From: The Proceedings of Mechanical Engineering Congress, Japan
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.
