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 amplitud...
| Những tác giả chính: | , |
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| Định dạng: | Journal article |
| Được phát hành: |
2004
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