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

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

Published:2018-06-24 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA/CEAS Aeroacoustics Conference
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Author:

Murayama Mitsuhiro¹,Yokokawa Yuzuru¹,Ito Yasushi¹,Takaishi Takehisa¹,Sakai Ryotaro¹,Yamamoto Kazuomi¹,Ueno Yosuke²,Isotani Kazuhide²,Tsuchimoto Yuta²,Hayama Kenji²,Hirai Tohru³,Tanaka Kentaro³

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. Kawasaki Heavy Industries, Ltd.

3. Ryoyu Systems Company, Ltd.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4085

Reference35 articles.

1. Imamura, T., Ura, H., Yokokawa, Y., Enomoto, S., Yamamoto, K., and Hirai, T. "Designing of Slat Cove Filler as a Noise Reduction Device for Leading-edge Slat," AIAA Paper 2007-3473.

2. Studies on Airframe Noise Generation at High-lift Devices in Relation to Aerodynamic Performances

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