Flow structure in controlled and baseline subsonic cavity flows

Jesse C Little, M. Debiasi, M. Samimy

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Abstract

This work presents preliminary results of an experimental investigation of the flow structure and acoustic signature in controlled and baseline subsonic cavity flows. Qualitative and quantitative data are presented and analyzed in an effort to better understand and predict the behavior of the shear layer over the cavity in response to various open-loop actuation cases. Experiments confirm that self-sustained flow-acoustic coupling occurs only at frequencies supporting an integer phase relationship around the flow-acoustic loop. Based on the results, we also speculate that only when the flow-acoustic components at frequencies supporting resonance are time-invariant can the corresponding coupling produces strong acoustic tones. Otherwise the corresponding flow-acoustic couplings produce multi-mode like resonance with tonal switching. This behavior is irrespective of the coherent structures passage frequency in the shear layer. This work is part of a larger multidisciplinary effort in the development and understanding of active feedback flow control techniques (Samimy et al. 2004).

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Pages5697-5714
Number of pages18
Volume8
StatePublished - 2006
Externally publishedYes
Event44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States
Duration: Jan 9 2006Jan 12 2006

Other

Other44th AIAA Aerospace Sciences Meeting 2006
CountryUnited States
CityReno, NV
Period1/9/061/12/06

Fingerprint

cavity flow
flow structure
Flow structure
cavity
acoustics
Acoustics
acoustic coupling
shear layers
flow control
actuation
Flow control
Feedback control
integers
signatures
cavities

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Little, J. C., Debiasi, M., & Samimy, M. (2006). Flow structure in controlled and baseline subsonic cavity flows. In Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting (Vol. 8, pp. 5697-5714)

Flow structure in controlled and baseline subsonic cavity flows. / Little, Jesse C; Debiasi, M.; Samimy, M.

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. Vol. 8 2006. p. 5697-5714.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Little, JC, Debiasi, M & Samimy, M 2006, Flow structure in controlled and baseline subsonic cavity flows. in Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. vol. 8, pp. 5697-5714, 44th AIAA Aerospace Sciences Meeting 2006, Reno, NV, United States, 1/9/06.
Little JC, Debiasi M, Samimy M. Flow structure in controlled and baseline subsonic cavity flows. In Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. Vol. 8. 2006. p. 5697-5714
Little, Jesse C ; Debiasi, M. ; Samimy, M. / Flow structure in controlled and baseline subsonic cavity flows. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. Vol. 8 2006. pp. 5697-5714
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