Analysis of liner performance using the NASA Langley Research Center Curved Duct Test Rig-Reference-Cited by-同舟云学术

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Analysis of liner performance using the NASA Langley Research Center Curved Duct Test Rig

Published:2016-01 Issue: Volume:102 Page:19-32
ISSN:0003-682X
Container-title:Applied Acoustics
language:en
Short-container-title:Applied Acoustics

Author:

Gerhold Carl H.,Brown Martha C.,Jones Michael G.,Howerton Brian M.

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference41 articles.

1. Envia E. Fan noise reduction: an overview. NASA TM-2001-210699; February 2001.

2. Silcox RJ. Experimental investigation of geometry and flow effects on acoustic radiation from duct inlets. AIAA paper 83-28012; 1983.

3. Ville JM, Silcox RJ. Experimental investigation of the radiation of sound from an unflanged duct and a bellmouth, including the flow effect. NASA-TP-1697; August 1, 1980.

4. Silcox RJ, Lester HC. Sound propagating through a variable area duct: experiment and theory. AIAA paper AIAA-81-1967; 1981.

5. Comparison of two waveguide methods for educing liner impedance in grazing flow;Jones;AIAA J,2004

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1. Framework for Modal Based Assessment of Liner Structures;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

2. Achieving cylindrical duct modes generation in spinning mode synthesizer via a least-square identification of the global calibration factor;Applied Acoustics;2022-01

3. Experimental comparison of noise dissipation effects of single- and double-layer acoustic liners;Applied Acoustics;2018-12

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