Sensitivity of the acoustics of short circular holes with bias flow to inlet edge geometries
File(s)GuzmanAIAA2019.pdf (3.79 MB)
Accepted version
Author(s)
Guzmán-Iñigo, Juan
Yang, Dong
Johnson, Holly G
Morgans, Aimee S
Type
Journal Article
Abstract
Short circular holes with a mean bias flow passing through them can absorb or generate acoustic energy depending on frequency. A recently proposed semi-analytical model (Yang and Morgans, Journal of Sound and Vibration, Vol. 384, 2016 pp. 294–311) based on the Green’s function method successfully captured this acoustic absorption and generation. The model pointed to the importance of accurately capturing the path followed by the unsteady vorticity shed from the hole inlet edge. In the present work, the effect of the path of the shed vorticity on the hole acoustics is systematically studied. The above model is combined with computational fluid dynamics tools for capturing how the path of the shed vorticity varies for small modifications in the hole inlet edge shape. A chamfered edge, a rounded edge, and two elliptical edge cases are considered to show that a very small change to the shape of the hole inlet edge can give rise to significant differences in the hole acoustic response.
Date Issued
2019-11
Date Acceptance
2019-05-17
Citation
AIAA Journal, 2019, 57 (11), pp.4835-4844
ISSN
0001-1452
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Start Page
4835
End Page
4844
Journal / Book Title
AIAA Journal
Volume
57
Issue
11
Copyright Statement
© 2019 by J. Guzmán-Iñigo, D. Yang, H. G. Johnson, and A. S. Morgans. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com ; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp .
Sponsor
Commission of the European Communities
Engineering & Physical Science Research Council (EPSRC)
Commission of the European Communities
Identifier
https://arc.aiaa.org/doi/10.2514/1.J057996
Grant Number
772080
EP/P003036/1
FP7 - 305410
Subjects
Science & Technology
Technology
Engineering, Aerospace
Engineering
HELMHOLTZ RESONATORS
PERFORATED PLATES
SOUND-ABSORPTION
IMPEDANCE
ORIFICE
DYNAMICS
LINERS
DUCT
Aerospace & Aeronautics
0901 Aerospace Engineering
0905 Civil Engineering
0913 Mechanical Engineering
Publication Status
Published
OA Location
https://doi.org/10.2514/1.J057996
Date Publish Online
2019-07-03