Volume 6: Structures and Dynamics, Parts a and B 2011
DOI: 10.1115/gt2011-46624
|View full text |Cite
|
Sign up to set email alerts
|

Mu Analysis for Turbomachinery Stall Flutter

Abstract: Flutter is an aeroelastic instability phenomenon that can result either in serious damage or complete destruction of a gas turbine blade structure. To assure a reliable and safe operation, potential for blade flutter must be eliminated from the turbo-machinery stages. In this paper, the robustness of an axial compressor blade design is studied with respect to parametric uncertainties through the Mu analysis. The analytical description of the nominal model used is based on matching a two dimensional incompressi… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Year Published

2022
2022
2022
2022

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
references
References 0 publications
0
0
0
Order By: Relevance