Analysis of the Effect of Mistuning on Turbomachinery Aeroelasticity
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منابع مشابه
Stabilization of Linear Flow Solver for Turbomachinery Aeroelasticity Using Recursive Projection Method
The linear analysis of turbomachinery aeroelasticity relies on the assumption of small level of unsteadiness and requires the solution of both the nonlinear steady and the linear unsteady flow equations. The objective of the analysis is to compute a complex flow solution that represents the amplitude and phase of the unsteady flow perturbation for the frequency of unsteadiness of interest. The ...
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