Lutter prediction of a transonic fan with travelling wave using fully coupled fluid/structure interaction

Hong Sik Im, GeCheng Zha

Research output: Chapter in Book/Report/Conference proceedingConference contribution

8 Citations (Scopus)

Abstract

This paper uses a fully coupled fluid/structure interaction (FSI) to investigate the flutter mechanism of a modern transonic fan rotor with a forward travelling wave. To in- duce an initial travelling wave for the blade structure, an initial BC that can facilitate each blade to vibrate with a time lag by a given nodal diameter (ND) is implemented. Unsteady Reynolds-averaged Navier-Stokes (URANS) equations are solved with a system of structure modal equations in a fully coupled manner. The 5th order WENO scheme with a low diffusion E-CUSP Riemann solver is used for the in- viscid fluxes and a 2nd order central differencing is used for the viscous terms. A half annulus sector is used for the flutter simulations with a time shifted phase lag boundary condition at the circumferential boundaries. The present FSI simulations show that the shock instability causes the flutter. When the detached normal shock moves further upstream in a direction normal to the blade chord, the interaction of the detached normal shock with tip leakage vortex creates more serious blockage to the blade passage that can introduce an aerodynamic instability to the blade structure due to the in- coming flow disturbance, resulting in flutter. The flutter of the transonic fan observed in this study occurs at the 1st mode before the stall. The predicted flutter boundary agrees well with the experiment.

Original languageEnglish
Title of host publicationProceedings of the ASME Turbo Expo
Volume7 B
DOIs
StatePublished - Dec 17 2013
EventASME Turbo Expo 2013: Turbine Technical Conference and Exposition, GT 2013 - San Antonio, Tx, United States
Duration: Jun 3 2013Jun 7 2013

Other

OtherASME Turbo Expo 2013: Turbine Technical Conference and Exposition, GT 2013
CountryUnited States
CitySan Antonio, Tx
Period6/3/136/7/13

Fingerprint

Fluid structure interaction
Fans
Phase boundaries
Navier Stokes equations
Aerodynamics
Vortex flow
Rotors
Boundary conditions
Fluxes
Experiments

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Lutter prediction of a transonic fan with travelling wave using fully coupled fluid/structure interaction. / Im, Hong Sik; Zha, GeCheng.

Proceedings of the ASME Turbo Expo. Vol. 7 B 2013. GT2013-94341.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Im, HS & Zha, G 2013, Lutter prediction of a transonic fan with travelling wave using fully coupled fluid/structure interaction. in Proceedings of the ASME Turbo Expo. vol. 7 B, GT2013-94341, ASME Turbo Expo 2013: Turbine Technical Conference and Exposition, GT 2013, San Antonio, Tx, United States, 6/3/13. https://doi.org/10.1115/GT2013-94341
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