- Abstract:
-
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 solution procedure of the linear harmonic Euler/Navier-Stokes solver of the HYDRA suite of codes cons...
Expand abstract - Publication status:
- Published
- Publisher copy:
- 10.2514/1.1225
-
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- Journal:
- AIAA JOURNAL
- Volume:
- 42
- Issue:
- 9
- Pages:
- 1765-1774
- Publication date:
- 2004-09-05
- DOI:
- EISSN:
-
1533-385X
- ISSN:
-
0001-1452
- URN:
-
uuid:922ef5eb-d5fb-4ecc-aa6c-89b9cd0e94af
- Source identifiers:
-
24274
- Local pid:
- pubs:24274
- Copyright date:
- 2004
Journal article
Stabilization of linear flow solver for turbomachinery aeroelasticity using recursive projection method
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