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Generation of unsteady CF-instability modes by vibrational and vibration-vortex localized receptivity mechanisms
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2018 (English)In: AIP Conference Proceedings, American Institute of Physics Inc. , 2018Conference paper, Published paper (Refereed)
Abstract [en]

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 low-turbulence 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 cwire, at frequencies of f s and f v , 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 f s . However, the evolution of the CF-modes excited at difference combination frequency f sv- = f s - f v 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 β′. This phenomenon was observed in the flow, which is stable with respect to both CF- and TS-waves having β′ = 0 for all frequencies. There is no explanation of this finding at present.

Place, publisher, year, edition, pages
American Institute of Physics Inc. , 2018.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-247078DOI: 10.1063/1.5065088ISI: 000481675800010Scopus ID: 2-s2.0-85056317829ISBN: 9780735417472 (print)OAI: oai:DiVA.org:kth-247078DiVA, id: diva2:1313438
Conference
19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, 13 August 2018 through 19 August 2018
Note

QC 20190503

Available from: 2019-05-03 Created: 2019-05-03 Last updated: 2019-09-05Bibliographically approved

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Örlü, RamisHanifi, Ardeshir

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