Abstract
In the blade design process, flow pattern prediction tools have an essential role to create a highly efficient blade shape. A viscous throughflow code, which can take into account the effects of boundary layer and blade thickness, was developed to evaluate axial turbine flows. In the present paper, the throughflow code is validated by applying it to a concentric annular tube flow. In addition* axial turbine internal flows were evaluated by the throughflow code. The simulation results showed that the throughflow code can predict the flow patterns very well if the effects of secondary flow are marginal.
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 the Fluids engineering conference
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.
