Abstract
This chapter develops a lattice-Boltzmann (LB) model capable of simulating turbo-machinery flows. In the past, LB method has not been applied to turbo-machines because of its Mach number limitations and inability to handle complex geometries effectively. In the recent work, one has successfully developed a high Mach number LB model that is capable of shock capturing. In the current paper, one concentrated on establishing the capability of handling complex geometries. To demonstrate the new capability, a simulation of transonic cascade flows by the compressible LB model is performed and reported here. The parallelization and parallel efficiency of the scheme is also discussed in this chapter.
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: Parallel Computational Fluid Dynamics 2001, Practice and Theory
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.
