Kentaro Tanaka

发表

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

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

Wiggle Controlled Turbulent Flow Simulations on Structured Grid at Low Mach Number

Kazuomi Yamamoto, Kentaro Tanaka, T. Hirai, 2018, 2018 AIAA/CEAS Aeroacoustics Conference.

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

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

JAXA’s Results of Fixed Grid RANS Simulations for the Fourth High Lift Prediction Workshop

Yasushi Ito, M. Murayama, Kentaro Tanaka, 2022, AIAA AVIATION 2022 Forum.

Multi-Objective Aerodynamic Optimization of Elements' Setting for High-lift Airfoil Using Kriging Model

Kazuomi Yamamoto, Masahiro Kanazaki, Shinkyu Jeong, 2006 .

Effect of Vortex Generators on Transonic Swept Wings

Shunsuke Koike, Kazuhiro Kusunose, Kazuomi Yamamoto, 2015 .

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

Mitsuhiro Murayama, Kazuomi Yamamoto, Akio Ochi, 2018 .

Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop

Kazuomi Yamamoto, Kentaro Tanaka, Mitsuhiro Murayama, 2015 .

Effect of a Nonlinear Constitutive Relation for Turbulence Modeling on Predicting Flow Separation at Wing-Body Juncture of Transonic Commercial Aircraft

Mitsuhiro Murayama, Kazuomi Yamamoto, Kentaro Tanaka, 2012 .

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 .

Comparison Study of Drag Prediction for the 4th CFD Drag Prediction Workshop using Structured and Unstructured Mesh Methods

Kazuomi Yamamoto, Kentaro Tanaka, Mitsuhiro Murayama, 2010 .

Far-Field Drag Analysis of NASA Common Research Model Simulation

Kazuomi Yamamoto, Kentaro Tanaka, Mitsuhiro Murayama, 2011 .

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

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

Summary of JAXA Studies for the Fifth AIAA CFD Drag Prediction Workshop Using UPACS and FaSTAR

Yasushi Ito, Kazuomi Yamamoto, Mitsuhiro Murayama, 2013 .

Summary of JAXA Studies for the 2nd AIAA CFD High Lift Prediction Workshop Using Structured and Unstructured Mesh CFD

Yasushi Ito, Mitsuhiro Murayama, Kazuomi Yamamoto, 2014 .

Turbulent Flow Solver Validation of FaSTAR and UPACS

Kazuomi Yamamoto, Mitsuhiro Murayama, Atsushi Hashimoto, 2014 .

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

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

Multi-Objective Aerodynamic Exploration of Elements’ Setting for High-Lift Airfoil Using Kriging Model

Kazuomi Yamamoto, Shinkyu Jeong, Masahiro Kanazaki, 2006 .

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.

High-Fidelity Aerodynamic Analysis of Aircraft in Various Configurations with MEGG3D

Mitsuhiro Murayama, Kazuomi Yamamoto, Yasushi Ito, 2017 .

Airframe Noise Reduction of Flap Side-edge Using Vortex Generators

Kazuomi Yamamoto, Yasushi Ito, Mitsuhiro Murayama, 2017 .

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.

CFD Comparison Study for Trapezoidal High-Lift Wing Configurations by Structured and Unstructured Mesh Method

Kazuomi Yamamoto, Kentaro Tanaka, Mitsuhiro Murayama, 2011 .

Analysis of the NASA Common Research Model Using the TAS Code and MEGG3D Grids

Yasushi Ito, Kazuomi Yamamoto, Mitsuhiro Murayama, 2017 .

Analysis using High-Order Schemes in Structured Grid CFD Solver, UPACS

Mitsuhiro Murayama, Kazuomi Yamamoto, Tohru Hirai, 2019 .

Effect of Vortex Generators on Transonic Swept Wings

Mitsuhiro Murayama, Shunsuke Koike, Kazuhiro Kusunose, 2015 .

Computational Efforts in Designing Experiment for High-lift Aeroacoustics

Yasushi Ito, Kazuomi Yamamoto, Mitsuhiro Murayama, 2013 .

Computational Studies of the NASA High-Lift Trap Wing Using Structured and Unstructured Grid Solvers

Yasushi Ito, Kazuomi Yamamoto, Kentaro Tanaka, 2012 .

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

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

TAS Code, FaSTAR, and Cflow Results for the Sixth Drag Prediction Workshop

Mitsuhiro Murayama, Kazuomi Yamamoto, Kentaro Tanaka, 2017, Journal of Aircraft.

TAS Code, FaSTAR and Cflow Results for the Sixth Drag Prediction Workshop

Yasushi Ito, Kazuomi Yamamoto, Mitsuhiro Murayama, 2017 .

Japan Aerospace Exploration Agency Studies for the Fifth AIAA Drag Prediction Workshop

Kazuomi Yamamoto, Kentaro Tanaka, Mitsuhiro Murayama, 2014 .

Computational Study on Porous-Plates for Reducing Airframe Noise Associated With Landing Gear Bay

M. Murayama, T. Takaishi, Kentaro Tanaka, 2024, 30th AIAA/CEAS Aeroacoustics Conference (2024).

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.