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Time-Domain Harmonic Balance Method for Turbomachinery Aeroelasticity

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Academic year: 2021

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Figure

Figure 1 shows the different states of the HB instants during the iteration process. Usually, all instants are initialized by the same initial condition (Fig
Fig. 2 STCF 11 mesh.
Fig. 5 Wall pressure harmonic analysis for an opposite phase vibration, subsonic case.
Fig. 8 Steady results of the isentropic Mach number at blade wall, transonic case.
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