Turbulent Boundary Layer Over Acoustic Liners

H. Shahzad; S. Hickel; D. Modesti

doi:10.1007/978-3-032-19268-4_14

Turbulent Boundary Layer Over Acoustic Liners

H. Shahzad
, S. Hickel^*
, D. Modesti

^*Corresponding author for this work

Aerodynamics

Research output: Chapter in Book/Conference proceedings/Edited volume › Chapter › Scientific › peer-review

Abstract

Aircraft engines are the primary source of noise during take-off and landing. To reduce noise emissions, passive noise control devices called acoustic liners cover the interior of engine nacelles. Acoustic liners consist of a honeycomb core, bounded by a porous top face-sheet and a solid backplate.

Original language	English
Title of host publication	Direct and Large Eddy Simulation XIV
Publisher	Springer Nature
Pages	92-97
Number of pages	6
DOIs	https://doi.org/10.1007/978-3-032-19268-4_14
Publication status	Published - 2026

Publication series

Name	ERCOFTAC Series
Volume	21
ISSN (Print)	1382-4309
ISSN (Electronic)	2215-1826

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10.1007/978-3-032-19268-4_14

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abstract = "Aircraft engines are the primary source of noise during take-off and landing. To reduce noise emissions, passive noise control devices called acoustic liners cover the interior of engine nacelles. Acoustic liners consist of a honeycomb core, bounded by a porous top face-sheet and a solid backplate.",

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AB - Aircraft engines are the primary source of noise during take-off and landing. To reduce noise emissions, passive noise control devices called acoustic liners cover the interior of engine nacelles. Acoustic liners consist of a honeycomb core, bounded by a porous top face-sheet and a solid backplate.

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BT - Direct and Large Eddy Simulation XIV

PB - Springer Nature

ER -

Turbulent Boundary Layer Over Acoustic Liners

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