- 2025
- 2024
-
- Development of Aircraft Noise Simulation Framework J-FRAIN Based on Component-Wise Sound Source Models
- Experimental and Numerical Investigation on Noise Directivity of the 30P30N Three-Element High-Lift Airfoil
- Computaional Study on Porous-Plates for Reducting Airframe Noise Associated With Landing Gear Bay
- Landing Gear Noise Reduction Using Porous Plates
- 2023
-
- FQUROHプロジェクトの成果と今後の活動（”Achievements of the FQUROH Project and Its Subsequent Activities”, in Japanese）
- TASによるCRM-HLの風洞壁を考慮したRANS定常空力解析（”Revnolds-averaged Navier-Stokes simulation of CRM-HL in wind tunnel using TAS code”, in Japanese）
- 騒音低減多孔板前・後配置の違いによる円柱周りの騒音低減効果の比較（”Comparison of noise reduction effect around a cylinder by forward and rearward porous plates”, in Japanese）
- Aircraft Noise Reduction Study on Inboard Slat-Tip Region
- A Numerical Study on Noise Generation Caused by Slat Tracks
- Study on Side-edge Geometry of Porous-Plate for Reduction of Airframe Noise from Landing Gear
- 2022
-
- Wind Tunnel Installation Effects on Japan Aerospace Exploration Agency's Standard Model
- Noise Reduction Design for High Lift Devices of Regional Jet
- Slat Noise Reduction Based on Turbulence Attenuation Downstream of Shear-layer Reattachment
- Effect of Slat Tracks and Inboard Slat Tip Geometry on Airframe Noise
- Further Noise Reduction of Regional Jet Two-Wheel Main Landing Gear
- 三菱航空機における航空機の低騒音化に対する取り組み（”Efforts to Reduce Aircraft Noise in Mitsubishi Aircraft Corporation”, in Japanese）
- リージョナルジェット機2輪主脚に対する低騒音化設計（” Low Noise Design of Regional Jet Two-Wheel Main Landing Gear ”, in Japanese）
- FQUROHプロジェクトにおける飛行実証試験（” Flight Demonstration Tests in the FQUROH Project”, in Japanese）
- リージョナルジェット機内舷スラットに対する低騒音化設計（” Noise Reduction Design for Inboard Slat of Regional Jet”, in Japanese）
- 2021
-
- JAXA機体騒音低減技術の研究開発(FQUROH+)における高揚力装置低騒音化研究（” Research of Technology to Reduce Airframe Noise from High Lift Devices in JAXA’s FQUROH+ R&D Program”, in Japanese）
- 飛翔フラップ表面圧力計測（”Flap Surface Pressure Measurements with ‘Hisho’”, in Japanese）
- 音源計測（” Sound Source Measurement’”, in Japanese）
- 機体騒音低減技術の飛行実証（FQUROH飛翔フェーズ）（” Flight Demonstration for Airframe Noise Reduction Technologies – FQUROH Project “Hisho” Phase”, in Japanese）
- 2020
-
- 飛翔低騒音化改造プロセスと飛行性能影響解析（” Process of Noise-Reduction Modification and Flight Performance Analysis for JAXA Experimental Aircraft”, in Japanese）
- 川崎重工業における機体騒音の研究開発（” Research and Development of Airframe Noise at Kawasaki Heavy Industries”, in Japanese）
- 飛翔に対する空力CFD 解析（”Computational Fluid Dynamics Simulations for JAXA Experimental Aircraft, Hisho”, in Japanese）
- 飛翔の大型低騒音風洞試験（” Acoustic Wind Tunnel Test with 18% scale Half-span Model of ‘Hisho’”, in Japanese）
- 主脚低騒音化デバイスの設計・製作（” NOISE REDUCTION DEVICE DESIGN AND PRODUCTION FOR MAIN LANDING GEAR”, in Japanese）
- 飛翔の主脚低騒音化（” Reduction of Airframe Noise from ‘Hisho’ Main Landing Gear’”, in Japanese）
- 飛翔のフラップ低騒音化（” Reduction of Airframe Noise from ‘Hisho’ Flap’”, in Japanese）
- 2019
-
- 機体騒音低減技術の飛行実証プロジェクトFQUROH の概要（” Overview of FQUROH : a Flight Demonstration Project for Airframe Noise Reduction Technologies”, in Japanese）
- 脚騒音低減多孔板の端部形状効果（”Side-edge effect of porous plate to improve noise reduction effect for landing gear”, in Japanese）
- JAXA's and KHI's Contributoin to the Third High Lift Prediction Workshop
- Computational Analysis of Noise Reduction Results for Flap Side-edges in the FQUROH Flight Demonstration Project
- Validation of Noise Reduction Design for Landing Gear in the FQUROH Flight Demonstration Project
- Noise Reduction of Regional Jet Two-Wheel Main Landing Gear
- Slat Noise Simulation on Unstructured Grid with Reduced Dissipation Approach
- 機体騒音低減技術の最近の研究開発動向とFQUROHプロジェクト（” Recent Research and Development of Noise Reduction Technologies and FQUROH Project”, in Japanese）
- 飛翔のフラップ低騒音化設計の検証（”Post Flight Demonstration Assessment on Flap Noise Reduction Design of “Hisho”.”, in Japanese）
- 飛翔の主脚低騒音化設計の検証（” Validation of Noise Reduction Design for Main Landing Gear of ‘Hisho’”, in Japanese）
- FQUROHプロジェクトにおけるスラット低騒音化に向けた空力音響シミュレーション（” Aeroacoustic Simulations for Slat Noise Reduction in FQUROH’”, in Japanese）
- Wind Tunnel Interference Effects on Japan Aerospace Exploration Agency's Standard Model
- Flap Surface Pressure Measurements with 3D printed Pressure Belts in FQUROH Flight Demonstration
- Numerical Simulation of Main Landing Gear Noise Reduction in FQUROH Flight Demonstraion
- Lattice-Boltzmann Simulation of the JAXA JSM High-Lift Configuration in a Wind Tunnel
- 2017
