A Theoretical Study on Aircraft Engine Acoustic Liner Optimization and Correlation with NASA Advanced Ducted Propulsor (ADP) Test-Reference-Cited by-同舟云学术

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A Theoretical Study on Aircraft Engine Acoustic Liner Optimization and Correlation with NASA Advanced Ducted Propulsor (ADP) Test

Published:2004-05-10 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Chien Eugene¹

Affiliation:

1. Goodrich Aerostructures Group

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3032

Reference102 articles.

1. Resistance R =0.2,0.5,and1.0

2. T D 42.80 0.087 0.37 42.52 0.104 0.22 R U -91.94 -0.060 0.20 -91.75 -0.065 0.12 0.2 M D 42.89 0.096 0.16 42.56 0.124 0.12

3. U -91.85 -0.046 0.10 -91.71 -0479 0.08 B D 42.96 0.103 - 42.61 0.129 -

4. U -91.76 -0.035 -91.64 -0404 -

5. T D 42.82 0.217 0.41 42.53 0.264 0.26 R U -91.94 -0.150 0.21 -91.75 -0.163 0.13 0.5 M D 42.92 0.240 0.17 42.58 0.314 0.10

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Engine Liner Optimization Using the Fast Scattering Code;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21

2. Comparison of Predicted and Measured Attenuation of Turbine Noise from a Static Engine Test;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21

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