Sensitive Flutter Parameters Analysis with Respect to Flutter-free Design of Compressor Blade

0Citations
Citations of this article
14Readers
Mendeley users who have this article in their library.

Abstract

As the mission requirements of the aero engine improve, the blade aerodynamic loading is higher, especially for lightweight designed blade. The possibility of the blade self-excited vibration increases, so flutter becomes one of the problems for fan and compressor design. However, there is no flutter related parametersin engineering as a reference for compressor flutter-free design until now. That is why the sensitive flutter parameters were studied which could suppress the flutter.

Cite

CITATION STYLE

APA

Hai, S., Lin, Y., & Hongxin, L. (2015). Sensitive Flutter Parameters Analysis with Respect to Flutter-free Design of Compressor Blade. In Procedia Engineering (Vol. 99, pp. 39–45). Elsevier Ltd. https://doi.org/10.1016/j.proeng.2014.12.505

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free