Y. Yokokawa

发表

OVERVIEW OF THE NUMERICAL SIMULATIONS OF A HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL

T. Imamura, Kazuomi Yamamoto, H. Ura, 2008 .

Phased Array Measurement of High Lift Devices in Low Speed Wind Tunnel

Takeshi Ito, H. Ura, Y. Yokokawa, 2006 .

High-Lift Device Testing in JAXA 6.5M X 5.5M Low-Speed Wind Tunnel

Takeshi Ito, Kazuomi Yamamoto, H. Ura, 2006 .

Numerical and Experimental Research of Low-Noise Slat Using Simplified High-lift Model

T. Imamura, Kazuomi Yamamoto, H. Ura, 2008 .

Three-Dimensional Unsteady Flow Computations Around a Conventional Slat of High-Lift Devices

T. Imamura, Kazuomi Yamamoto, Y. Yokokawa, 2008 .

VALIDATION STUDY OF CFD ANALYSIS FOR HIGH-LIFT SYSTEMS

M. Murayama, Kazuomi Yamamoto, Y. Yokokawa, 2006 .

Investigation of Near-field Flow Unsteadiness around a NACA0012 Wingtip using Large-Eddy-Simulation Approach

T. Imamura, Kazuomi Yamamoto, Y. Yokokawa, 2010 .

S0505-3-5 An Investigation on Airframe Noise Sources of Landing Gear Model

Kazuomi Yamamoto, Yuzuru Yokokawa, Hiroki Ura, 2009 .

Computational study of low-noise fairings around tire-axle region of a two-wheel main landing gear

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2013 .

Lattice-Boltzmann Flow Simulation of a Two-Wheel Landing Gear

M. Murayama, E. Manoha, Laurent Sanders, 2016 .

Wind Tunnel Interference Effects on Japan Aerospace Exploration Agency’s Standard Model

Mitsuhiro Murayama, Kazuomi Yamamoto, Kentaro Tanaka, 2019, AIAA Scitech 2019 Forum.

A Far-field Noise and Near-field Unsteadiness of a Simplified High-lift-configuration Model (Flap-edge)

T. Imamura, Kazuomi Yamamoto, H. Ura, 2009 .

Japan Aerospace Exploration Agency’s and Kawasaki Heavy Industries’ Contribution to the Third High Lift Prediction Workshop

Mitsuhiro Murayama, Kazuomi Yamamoto, Akio Ochi, 2018 .

Aerodynamic Influence of a Half-Span Model Installation for High-Lift Configuration Experiment

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2010 .

Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2008 .

Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing

Kazuomi Yamamoto, Masahiro Kanazaki, Mitsuhiro Murayama, 2008 .

Experiment and CFD of a High-lift Configuration Civil Transport Aircraft Model

Mitsuhiro Murayama, Kazuomi Yamamoto, Takeshi Ito, 2006 .

Nacelle Chine Installation Based on Wind-Tunnel Test Using Efficient Global Optimization

Kazuomi Yamamoto, Mitsuhiro Murayama, Takeshi Ito, 2008 .

JAXA’s and KHI’s Contribution to the Third High Lift Prediction Workshop

Mitsuhiro Murayama, Kazuomi Yamamoto, Kentaro Tanaka, 2019, Journal of Aircraft.

Computational and Experimental Study on Noise Generation from Tire-Axle Regions of a Two-Wheel Main Landing Gear

Long Wu, Kazuomi Yamamoto, Mitsuhiro Murayama, 2011 .

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

Yasushi Ito, M. Murayama, T. Takaishi, 2017, 2018 AIAA/CEAS Aeroacoustics Conference.

Numerical Simulation of a Two-Wheel Main Landing Gear with Low-Noise Fairings around Tire-Axle Region

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2012 .

Aeroacoustic Simulation of JAXA Landing Gear by Building-Cube Method and Non-compact Curle's Equation

Kazuhiro Nakahashi, Daisuke Sasaki, Kazuomi Yamamoto, 2012 .

COMPUTATIONAL STUDY ON NOISE GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR

M. Murayama, Y. Yokokawa, K. Yamamoto, 2012 .

Aerodynamic and aeroacoustic simulations of a two-wheel landing gear

Kazuomi Yamamoto, Yuzuru Yokokawa, Tohru Hirai, 2010 .

Reprint of: Aerodynamic and Aeroacoustic Simulations of a Two-wheel Landing Gear

Kazuomi Yamamoto, Yuzuru Yokokawa, Tohru Hirai, 2010 .

Numerical Analysis of Steady Flow around a Landing Gear Noise Measurement Model

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2009 .

COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA

M. Murayama, Takeshi Ito, Y. Yokokawa, 2008 .

Aerodynamics of High-Lift Configuration Civil Aircraft Model in JAXA

Kazuomi Yamamoto, Mitsuhiro Murayama, Takeshi Ito, 2007 .

Noise Source Analysis of Aircraft Flyover Test Based on Time Domain Beamforming Method

Kazuomi Yamamoto, Yuzuru Yokokawa, Takehisa Takaishi, 2016 .

High-resolution Fly-over Beamforming Using a Small Practical Array

Tatsuya Ishii, Kazuomi Yamamoto, Yuzuru Yokokawa, 2012 .

Noise Reduction of Regional Jet Two-Wheel Main Landing Gear

Yasushi Ito, T. Takaishi, Y. Yokokawa, 2019, 25th AIAA/CEAS Aeroacoustics Conference.

Validation of Noise Reduction Design for Landing Gear in the FQUROH Flight Demonstration Project

Yasushi Ito, Kazuomi Yamamoto, Mitsuhiro Murayama, 2019, Advanced Courses.

Computational Analysis of Noise Reduction Results for Flap Side-edges in the FQUROH Flight Demonstration Project

Ryotaro Sakai, Yasushi Ito, Kazuomi Yamamoto, 2019, 25th AIAA/CEAS Aeroacoustics Conference.

FQUROH: A Flight Demonstration Project for Airframe Noise Reduction Technology – the 2nd Flight Demonstration

Ryotaro Sakai, Kazuomi Yamamoto, Mitsuhiro Murayama, 2017, 2018 AIAA/CEAS Aeroacoustics Conference.

Acoustic Wind Tunnel Test with 18% Scale Half-span Model toward FQUROH Second Flight Demonstration

Yasushi Ito, M. Murayama, T. Takaishi, 2017, 2018 AIAA/CEAS Aeroacoustics Conference.

Airframe noise measurements on JAXA Jet Flying Test Bed “Hisho” using a phased microphone array

Ryotaro Sakai, Kazuomi Yamamoto, Mitsuhiro Murayama, 2017 .

An Aerodynamic Noise Reduction Study for Airframe Noise from Flap Tips

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2013 .

Experimental study on Noise Generation of a Two-Wheel Main Landing Gear

Kazuomi Yamamoto, Yuzuru Yokokawa, Hiroki Ura, 2010 .

Aerodynamic/Aeroacoustic testing in Anechoic Closed Test Sections of Low-speed Wind Tunnels

Ricardo A. Burdisso, Wing Ng, Kazuomi Yamamoto, 2010 .

Airframe Noise Reduction of Flap Side-edge Using Vortex Generators

Kazuomi Yamamoto, Yasushi Ito, Mitsuhiro Murayama, 2017 .

Noise Reduction Design for High Lift Devices of Regional Jet

Yasushi Ito, M. Murayama, T. Takaishi, 2022, 28th AIAA/CEAS Aeroacoustics 2022 Conference.

Noise Reduction Design for Landing Gear toward FQUROH Flight Demonstration

Kazuomi Yamamoto, Mitsuhiro Murayama, Yasushi Ito, 2017 .

Noise Generation Characteristics of a High-lift Swept and Tapered Wing Model

Shigemi Shindo, Kazuomi Yamamoto, Mitsuhiro Murayama, 2013 .

Numerical Investigation on Change of Airframe Noise by Flap Side-edge Shape

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2013 .

CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model

Mitsuhiro Murayama, Kazuomi Yamamoto, Yuzuru Yokokawa, 2007 .

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

Ryotaro Sakai, Kazuomi Yamamoto, Mitsuhiro Murayama, 2017, Advanced Courses.

Numerical Simulation of Main Landing Gear Noise Reduction in FQUROH Flight Demonstration

Yasushi Ito, M. Murayama, T. Takaishi, 2019, AIAA Scitech 2019 Forum.

Further Noise Reduction Design for Landing Gear toward FQUROH Second Flight Demonstration

Ryotaro Sakai, Kazuomi Yamamoto, Mitsuhiro Murayama, 2018, 2018 AIAA/CEAS Aeroacoustics Conference.

Flyover Array Measurements with JAXA Flying Test Bed ‘Hisho’

Ryotaro Sakai, Kazuomi Yamamoto, Mitsuhiro Murayama, 2016 .

Study on Change of Noise Generation from Slat Track Shape

Kazuomi Yamamoto, Yasushi Ito, Mitsuhiro Murayama, 2016 .

Study on Noise Generation from Slat Tracks Using a High-Lift Wing Model

Kazuomi Yamamoto, Mitsuhiro Murayama, Yasushi Ito, 2015 .

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

Kazuomi Yamamoto, Takeshi Ito, Yuzuru Yokokawa, 2008 .

Designing of Slat Cove Filler as a Noise Reduction Device for Leading-edge Slat

Kazuomi Yamamoto, Yuzuru Yokokawa, Hiroki Ura, 2007 .

Lattice-Boltzmann Simulations of the JAXA JSM High-Lift Configuration in a Wind Tunnel

Kazuomi Yamamoto, Mitsuhiro Murayama, Yasushi Ito, 2019, AIAA Scitech 2019 Forum.

Investigation of Noise Generation from Bluff Flap Side-edge of a High-Lift Wing Model

Shigemi Shindo, Hiroshi Kobayashi, Kazuomi Yamamoto, 2014 .

Computational Efforts in Designing Experiment for High-lift Aeroacoustics

Yasushi Ito, Kazuomi Yamamoto, Mitsuhiro Murayama, 2013 .

Acoustic Wind Tunnel Test with 18% Scale Half-span Model toward FQUROH Second Flight Demonstration

Ryotaro Sakai, Kazuomi Yamamoto, Mitsuhiro Murayama, 2017, Advanced Courses.

A Far-field Noise and Near-field Unsteadiness of a Simplified High-lift-configuration Model (Slat)

Kazuomi Yamamoto, Yuzuru Yokokawa, Hiroki Ura, 2009 .

Experimental Study of Slat Noise from 30P30N Three-Element High-Lift Airfoil in JAXA Kevlar-Wall Low-Speed Wind Tunnel

K. Nakakita, Yasushi Ito, M. Murayama, 2018, Advanced Courses.

AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS

Takeshi Ito, H. Ura, Y. Yokokawa, 2008 .

Wind Tunnel Installation Effects on Japan Aerospace Exploration Agency’s Standard Model

Yasushi Ito, M. Murayama, Y. Yokokawa, 2022, Journal of Aircraft.

Evaluation of Computations and Transition Prediction Method for Aircraft High-Lift Configuration

Kazuomi Yamamoto, Mitsuhiro Murayama, Yuzuru Yokokawa, 2009 .

Flap -edge Flowfield and Noise in Civil Transport Aircraft Model

Kazuhiro Nakahashi, Mitsuhiro Murayama, Yuzuru Yokokawa, 2007 .

PIV Investigation of Nacelle Chine Effects on High-Lift System Performance

Mitsuhiro Murayama, Takeshi Ito, Yuzuru Yokokawa, 2008 .

Efficient Design Exploration of Nacelle Chine Installation in Wind Tunnel Testing

Mitsuhiro Murayama, Kazuomi Yamamoto, Takeshi Ito, 2008 .

Progress on Experimental and Numerical Research for Slat Noise in JAXA

Kazuomi Yamamoto, Yuzuru Yokokawa, Taro Imamura, 2011 .

Numerical Simulation of NACA0012 Wingtip Flow Leading to Noise Generation

Kazuomi Yamamoto, Yuzuru Yokokawa, Taro Imamura, 2005 .

1802 High-lift Airfoil Design for a Take-Off Configuration Using Kriging Based GA

Kazuomi Yamamoto, Mitsuhiro Murayama, Masahiro Kanazaki, 2007 .

W101 Fluorescent Oil Flow Visualization in Aircraft Research Experiment

Kazuomi Yamamoto, Yuzuru Yokokawa, Hiroshi Uchida, 2009 .

Study on Side-edge Geometry of Porous-Plate for Reduction of Airframe Noise from Landing Gear

Yasushi Ito, M. Murayama, T. Takaishi, 2023, AIAA AVIATION 2023 Forum.