Quasi Three-Dimensional Flutter Analysis of Single-row STCF4 Turbine Blade Cascade in Supersonic Flow
Date
2013
Authors
Advisors
Journal Title
Journal ISSN
Volume Title
Repository Usage Stats
387
views
views
1190
downloads
downloads
Abstract
In this work the interaction of flutter-a self-excited self-sustained aeroelastic vibration phenomenon-with wake excitation is investigated using a harmonic balance frequency domain CFD code to solve the 2D inviscid Euler equations for a rotor in choke flutter operation. The wake deficit and the blade-motion amplitude (torsion) are varied.
Type
Department
Description
Provenance
Citation
Permalink
Citation
Yin, Jiadong (2013). Quasi Three-Dimensional Flutter Analysis of Single-row STCF4 Turbine Blade Cascade in Supersonic Flow. Master's thesis, Duke University. Retrieved from https://hdl.handle.net/10161/7324.
Collections
Dukes student scholarship is made available to the public using a Creative Commons Attribution / Non-commercial / No derivative (CC-BY-NC-ND) license.