Noise Reduction Design for Flap Side-edges toward FQUROH Flight Demonstration-Reference-Cited by-同舟云学术

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Noise Reduction Design for Flap Side-edges toward FQUROH Flight Demonstration

Published:2017-06-02 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Murayama Mitsuhiro¹,Yamamoto Kazuomi¹,Yokokawa Yuzuru¹,Ito Yasushi¹,Takaishi Takehisa¹,Hirai Tohru²,Tanaka Kentaro²

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. Ryoyu Systems Company, Ltd.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4031

Reference39 articles.

1. An Assessment of Flap and Main Landing Gear Noise Abatement Concepts

2. Evaluation of Airframe Noise Reduction Concepts via Simulations Using a Lattice Boltzmann Approach

Cited by 10 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. Noise Reduction Design for High Lift Devices of Regional Jet;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

2. Computational Analysis of Noise Reduction Results for Flap Side-edges in the FQUROH Flight Demonstration Project;25th AIAA/CEAS Aeroacoustics Conference;2019-05-18

3. A flight demonstration for airframe noise reduction technology;CEAS Aeronautical Journal;2019-03

4. Acoustic Wind Tunnel Test with 18% Scale Half-span Model toward FQUROH Second Flight Demonstration;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24

5. Noise Reduction Design for Flap Side-edges toward FQUROH Second Flight Demonstration;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24

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