Abstract
A numerical simulation was conducted using the commercial computational fluid dynamics software FLUENT to study the influence of inner flow structures on the motion characteristics of a separation oblique shock train caused by backpressure. Simulation results indicated there was a separation point of the boundary layer at the head of the shock train. The separated flow expanded in the isolator and led to movements of the shock train. With the shock train moving forward in the isolator, the leading edge of the shock train passed through the peaks and valleys of pressure along the forward path. As the pressure gradient at the separation point switched between positive and negative gradients, the state properties of the shock train movements transformed between a slow forward movement and a sudden sharp forward movement. The sudden sharp forward movement of the shock train always occurred when the separation point surmounted reflection points of the background wave system, which implies that the forward motion characteristics of shock train are related to the background flow structures. So, the occurrence of a sharp forward movement of the shock train can be predicted from the flow structures of a fully started state.
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.