The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses
We study the fluid–structure interaction (FSI) of a compliant panel with developing Blasius boundary-layer flow. The linearised Navier–Stokes equations in velocity–vorticity form are solved using a Helmholtz decomposition coupled with the dynamics of a plate-spring compliant panel couched in finite-...
| Main Authors: | , |
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| Format: | Journal Article |
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Cambridge University Press
2017
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| Online Access: | http://hdl.handle.net/20.500.11937/56987 |
| _version_ | 1848759986757304320 |
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| author | Tsigklifis, Konstantinos Lucey, A. |
| author_facet | Tsigklifis, Konstantinos Lucey, A. |
| author_sort | Tsigklifis, Konstantinos |
| building | Curtin Institutional Repository |
| collection | Online Access |
| description | We study the fluid–structure interaction (FSI) of a compliant panel with developing Blasius boundary-layer flow. The linearised Navier–Stokes equations in velocity–vorticity form are solved using a Helmholtz decomposition coupled with the dynamics of a plate-spring compliant panel couched in finite-difference form. The FSI system is written as an eigenvalue problem and the various flow- and wall-based instabilities are analysed. It is shown that global temporal instability can occur through the interaction of travelling wave flutter (TWF) with a structural mode or as a resonance between Tollmien–Schlichting wave (TSW) instability and discrete structural modes of the compliant panel. The former is independent of compliant panel length and upstream inflow disturbances while the specific behaviour arising from the latter phenomenon is dependent upon the frequency of a disturbance introduced upstream of the compliant panel. The inclusion of axial displacements in the wall model does not lead to any further global instabilities. The dependence of instability-onset Reynolds numbers with structural stiffness and damping for the global modes is quantified. It is also shown that the TWF-based global instability is stabilised as the boundary layer progresses downstream while the TSW-based global instability exhibits discrete resonance-type behaviour as Reynolds number increases. At sufficiently high Reynolds numbers, a globally unstable divergence instability is identified when the wavelength of its wall-based mode is longer than that of the least stable TSW mode. Finally, a non-modal analysis reveals a high level of transient growth when the flow interacts with a compliant panel which has structural properties capable of reducing TSW growth but which is prone to global instability through wall-based modes. |
| first_indexed | 2025-11-14T10:08:36Z |
| format | Journal Article |
| id | curtin-20.500.11937-56987 |
| institution | Curtin University Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-14T10:08:36Z |
| publishDate | 2017 |
| publisher | Cambridge University Press |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | curtin-20.500.11937-569872019-02-19T05:36:14Z The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses Tsigklifis, Konstantinos Lucey, A. We study the fluid–structure interaction (FSI) of a compliant panel with developing Blasius boundary-layer flow. The linearised Navier–Stokes equations in velocity–vorticity form are solved using a Helmholtz decomposition coupled with the dynamics of a plate-spring compliant panel couched in finite-difference form. The FSI system is written as an eigenvalue problem and the various flow- and wall-based instabilities are analysed. It is shown that global temporal instability can occur through the interaction of travelling wave flutter (TWF) with a structural mode or as a resonance between Tollmien–Schlichting wave (TSW) instability and discrete structural modes of the compliant panel. The former is independent of compliant panel length and upstream inflow disturbances while the specific behaviour arising from the latter phenomenon is dependent upon the frequency of a disturbance introduced upstream of the compliant panel. The inclusion of axial displacements in the wall model does not lead to any further global instabilities. The dependence of instability-onset Reynolds numbers with structural stiffness and damping for the global modes is quantified. It is also shown that the TWF-based global instability is stabilised as the boundary layer progresses downstream while the TSW-based global instability exhibits discrete resonance-type behaviour as Reynolds number increases. At sufficiently high Reynolds numbers, a globally unstable divergence instability is identified when the wavelength of its wall-based mode is longer than that of the least stable TSW mode. Finally, a non-modal analysis reveals a high level of transient growth when the flow interacts with a compliant panel which has structural properties capable of reducing TSW growth but which is prone to global instability through wall-based modes. 2017 Journal Article http://hdl.handle.net/20.500.11937/56987 10.1017/jfm.2017.453 Cambridge University Press fulltext |
| spellingShingle | Tsigklifis, Konstantinos Lucey, A. The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses |
| title | The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses |
| title_full | The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses |
| title_fullStr | The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses |
| title_full_unstemmed | The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses |
| title_short | The interaction of Blasius boundary-layer flow with a compliant panel: global, local and transient analyses |
| title_sort | interaction of blasius boundary-layer flow with a compliant panel: global, local and transient analyses |
| url | http://hdl.handle.net/20.500.11937/56987 |