Abstract
Cascade tests on a set-up equipped with converging lateral walls are more representative of the flow in a section of actual turbomachine than in those with two-dimensional-flow. The experiment is carried out at mid-span, where it is necessary to know the local area contraction evolution in order to get more representative data: for this purpose, a simple computation method has been developed and successfully applied, as shown by the comparison with experimental data. By means of successive approaches, the side wall shape can be defined so that a given area contraction evolution can be obtained at the center.
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 callDisclaimer: 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.
