Journal article icon

Journal article

Stabilization of linear flow solver for turbomachinery aeroelasticity using recursive projection method

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

Actions


Access Document


Publisher copy:
10.2514/1.1225

Authors


Campobasso, MS More by this author
More by this author
Institution:
University of Oxford
Department:
Oxford, MPLS, Mathematical Inst
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

Terms of use


Metrics



If you are the owner of this record, you can report an update to it here: Report update to this record

TO TOP