Abstract
An experimental investigation of the slow speed performance of a tandem cascade of aerofoils is described. The theoretical criteria on which the cascade was designed are discussed; the method of Ackeret, described elsewhere, was used to obtain the geometry of the aerofoils. Tests were carried out on the effect of the magnitude of the gap between each tandem pair and of the effect of varying, independently, the stagger of each aerofoil. Tests were carried out over a wide range of inlet angle for the range of staggers adopted and optimum deflections for the cascade were determined.
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 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.
