Research Article

Fluid-Thermal-Structural Coupled Analysis of a Radial Inflow Micro Gas Turbine Using Computational Fluid Dynamics and Computational Solid Mechanics

Figure 16

Distribution of dimensionless equivalent stress on the turbine blade.
640560.fig.0016a
(a) Distribution of dimensionless equivalent stress with thermal load considered
640560.fig.0016b
(b) Distribution of dimensionless equivalent stress with centrifugal load and aerodynamic load considered
640560.fig.0016c
(c) Distribution of dimensionless equivalent stress with centrifugal load, aerodynamic load, and thermal load considered