Kachanov, Y. S. and Borodulin, V. I. and Ivanov, A. V. and Mischenko, D. A. and Örlü, R. and Hanifi, Ardeshir and Hein, Stefan (2018) Generation of unsteady CF-instability modes by vibrational and vibration-vortex localized receptivity mechanisms. In: AIP Conference Proceedings, 2027 (020010). American Institute of Physics. 19th International Conference on the Methods of Aerophysical Research (ICMAR), 2018-08-13 - 2018-08-19, Novosibirsk, Russia. doi: 10.1063/1.5065088.
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Official URL: https://doi.org/10.1063/1.5065088
Abstract
The paper is based on results obtained within an international project ‘RECEPT’ of the European Framework Program FP7. The experiments were carried out in a three-dimensional boundary layer developing on an experimental model of a long-laminar-run swept airfoil (sweep angle of 35°). The model was mounted in a test section of the lowturbulence wind-tunnel MTL (KTH, Stockholm) at an angle of attack of −5° and equipped with sidewalls provided satisfaction of infinite-span conditions. The cross-flow (CF) instability modes were predominant in this case, while the Tollmien–Schlichting (TS) waves were suppressed by a favorable pressure gradient. The main measurements were carried out by means of hot-wire anemometry at conditions of excitation of fully controlled, unsteady surface and flow perturbations. These perturbations were excited by special sources: (1) a row of oscillating membranes and (2) a vibrating wire, at frequencies of fs and fv, respectively. A very good, quantitative agreement between the measured and calculated (by linear stability theory based on PSE approach) amplification curves was found at surface frequency fs. However, the evolution of the CF-modes excited at difference combination frequency fsv– = fs – fv turned out to be very much different from the theoretical one. Thorough analysis of the obtained results has shown that the only explanation of these discrepancies can be associated with presence of a distributed receptivity mechanism due to scattering of freestream vortices on the CF-instability waves excited by surface vibrations. Another unusual and unexpected phenomenon found in the present experiments is associated with anomalous amplification of difference combination modes with the zero spanwise wavenumbers E′. This phenomenon was observed in the flow, which is stable with respect to both CF- and TSwaves having E′ = 0 for all frequencies. There is no explanation of this finding at present.
| Item URL in elib: | https://elib.dlr.de/118590/ | ||||||||||||||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||||||||||
| Title: | Generation of unsteady CF-instability modes by vibrational and vibration-vortex localized receptivity mechanisms | ||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | 2 November 2018 | ||||||||||||||||||||||||||||||||
| Journal or Publication Title: | AIP Conference Proceedings | ||||||||||||||||||||||||||||||||
| Refereed publication: | No | ||||||||||||||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||||||||||||||
| Volume: | 2027 | ||||||||||||||||||||||||||||||||
| DOI: | 10.1063/1.5065088 | ||||||||||||||||||||||||||||||||
| Publisher: | American Institute of Physics | ||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||
| Keywords: | laminar-turbulent transition, three-dimensional boundary layer, EU project RECEPT | ||||||||||||||||||||||||||||||||
| Event Title: | 19th International Conference on the Methods of Aerophysical Research (ICMAR) | ||||||||||||||||||||||||||||||||
| Event Location: | Novosibirsk, Russia | ||||||||||||||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||||||||||||||
| Event Start Date: | 13 August 2018 | ||||||||||||||||||||||||||||||||
| Event End Date: | 19 August 2018 | ||||||||||||||||||||||||||||||||
| Organizer: | American Institute of Physics | ||||||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Flight Physics (old) | ||||||||||||||||||||||||||||||||
| Location: | Göttingen | ||||||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO | ||||||||||||||||||||||||||||||||
| Deposited By: | Hein, Dr.-Ing. Stefan | ||||||||||||||||||||||||||||||||
| Deposited On: | 27 Sep 2018 13:43 | ||||||||||||||||||||||||||||||||
| Last Modified: | 24 Apr 2024 20:22 |
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