Noise Reduction Potential through Slat Hook Serrations-Reference-Cited by-同舟云学术

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Noise Reduction Potential through Slat Hook Serrations

Published:2011-06-05 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference)
language:
Short-container-title:

Author:

Kopiev Victor¹,Zaitsev Mikhail¹,Belyaev Ivan¹,Mironov Mikhail²

Affiliation:

1. TsAGI

2. Andreev Acoustic Institute

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2909

Reference11 articles.

1. Almost 40 Years of Airframe Noise Research: What Did We Achieve?

2. ChowL.C. etal., Landinggears and highlift devices airframenoiseresearch,2002, AIAA Paper2002-2408.

3. Rackl, R. R., Miller, G., Guo, Y., and Yamamoto, K. "Airframe Noise Studies - Review and Future Direction",NASA report NASA/CR-2005-213767,2005

4. Slat noise source studies for farfield noise prediction

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2. Experimental Study of Far-Field Aerodynamic Noise Characteristics of Serrated Slat;Journal of Aerospace Engineering;2023-01

3. Slat noise control using active piezo-ceramic actuator;International Journal of Computer Applications in Technology;2023

4. Effects of Porous Gap Fillers on 30P30N Leading-Edge Slat Noise. Part I: Surface Pressure and Acoustics;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

5. Assessment of Slat Extensions and a Cove Filler for Slat Noise Reduction;AIAA Journal;2021-12

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