Abstract
The paper reports an extension of the double linearization theory to study effects of mean angle of attack, camber and thickness on flutter of a rotating subsonic annular cascade of blades. Numerical results compared with the strip theory prediction are presented to demonstrate some features of three-dimensional effects. It is found that the three-dimensional effect is essentially important. The strip theory approximation overestimates the spanwise variation of aerodynamic forces on vibrating blades, and in some cases, underestimates the overall aerodynamic work due to the mean loading.
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: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
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.
