Time-Domain Harmonic Balance Method for Turbomachinery Aeroelasticity
نویسندگان
چکیده
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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ژورنال
عنوان ژورنال: AIAA Journal
سال: 2014
ISSN: 0001-1452,1533-385X
DOI: 10.2514/1.j051848