Abstract

In this paper an improved mathematical formulation is given of the double linearization theory for predicting the mean loading effect upon the unsteady aerodynamic force for two-dimensional vibrating cascades in subsonic flows. The double linearization theory deals with both steady and unsteady components of disturbances on the basis of a linearized approximation on the assumption that the cascade is lightly loaded and vibrating with an infinitesimal displacement amplitude. The improvement is to take account of the effect of equivalent unsteady mass sources due to motion of blades with a steady fluid density jump between the upper and lower surfaces of blades. Unsteady aerodynamic forces on lightly loaded cascades predicted by the present theory show good agreement with predictions by numerical field methods and experimental data. The dependence of the flutter boundary upon cascade design parameters is demonstrated.

Full Text
Paper version not known

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 call

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.