Abstract
The results of tests on a series of small inward radial flow turbines, reported by Hiett and Johnston, are analysed. Stagnation type pressure loss coefficients are established for the rotors, enabling their performance to be predicted with fair accuracy over a wide range of operating conditions in both directions of rotation. In particular, secondary losses are related to the forces acting on the vanes, using a similar method to that of Ainley and Mathieson for axial flow turbines. Additional losses occurring during reverse rotation are related to the variation of lift coefficient with radius in the exducer.
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: Proceedings of the Institution of Mechanical Engineers, Conference Proceedings
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.
