Performance Evaluation of Cascade Considering Fluid/Structure Coupling Deformation

유체/구조 연계 변형효과를 고려한 케스케이드의 성능평가

  • 오세원 (국립경상대학교 기계항공공학부 대학원) ;
  • 김동현 (국립경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 김유성 (국립경상대학교 기계항공공학부 대학원) ;
  • 박웅 (두산중공업(주) 기술연구원)
  • Published : 2007.05.10

Abstract

In this study, a fluid-structure interaction (FSI) analysis system has been developed in order to evaluate the turbine cascade performance with blade structural deformation effect. Relative movement of the rotor with respect to stator is reflected by modeling independent two computational domains. To consider the deformed position of rotor airfoil, dynamic moving grid method is applied. Reynolds-averaged Navier-Stokes equations with one equation Spalart-Allmaras and two-equation SST $k-{\varepsilon}$ turbulence models are solved to predict unsteady fluid dynamic loads. A fully implicit time marching scheme based on the Newmark direct integration method with high artificial damping is used to compute the fluid-structure interaction problem. Cascade performance evaluations for different elastic axis positions are presented and compared each other. It is importantly shown that the predicted aerodynamic performance considering structural deformation effect of blade can show some deviations compared to the data generally computed from rigid blade configurations and the position of elastic axis also tend to give sensitive effect.

Keywords