Kenji Yoshida

发表

Development of Inverse Design System for Supersonic Natural Laminar Flow Wing on High Reynolds Number Condition

Yoshine Ueda, Hiroaki Ishikawa, Naoko Tokugawa, 2016 .

Boundary Layer Transition Measurement using Preston tube on NEXST-1 Flight Test

Hiroaki Ishikawa, Dong-Youn Kwak, Masayoshi Noguchi, 2007 .

Study on flow-pattern identification method using pressure drop characteristics of gas-liquid flow in narrow channel

Kenji Yoshida, Isao Kataoka, Tatsunori Konishi, 2012 .

Subchannel Analysis with Mechanistic Methods for Thermo-Hydro Dynamics in BWR Fuel Bundles

Kenji Yoshida, Masanori Naitoh, Isao Kataoka, 2006 .

Numerical Analysis on Flight-Test Results of Supersonic Experimental Airplane NEXST-1

Hiroaki Ishikawa, Dong-Youn Kwak, Kenji Yoshida, 2007 .

Mechanistic Prediction of CHF in Fuel Assembly Using the Subchannel Code CAPE

Kenji Yoshida, Isao Kataoka, Masanori Naito, 2009 .

Mechanistic Prediction of Void Fraction Distribution in BWR Fuel Assembly Using the Subchannel Code CAPE

Kenji Yoshida, Masanori Naitoh, Isao Kataoka, 2009 .

Experimental and numerical study for aerodynamics of low boom configuration

Kenji Yoshida, 1994 .

Flight Test Measurements of Surface Pressure on Unmanned Scaled Supersonic Experimental Airplane

Dong-Youn Kwak, Masayoshi Noguchi, Hiroaki Ishikawa, 2006 .

Research on Drag Reduction in Hydraulic System of Construction Machines

Kenji Yoshida, Kenji Yoshida, 2013 .

Transient local extinction and reignition behavior of diffusion flames affected by flame curvature and preferential diffusion

Toshimi Takagi, Kenji Yoshida, Kenji Yoshida, 1998 .

Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number Conditions

Kisa Matsushima, Yoshine Ueda, Hiroaki Ishikawa, 2014 .

Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1

Dong-Youn Kwak, Yoshine Ueda, Naoko Tokugawa, 2008 .

ADVERSE REYNOLDS NUMBER EFFECT ON MAXIMUM LIFT OF TWO DIMENSIONAL AIRFOILS

Masayoshi Noguchi, Kenji Yoshida, 2000 .

Nonlinear Analysis of the First-Mode Dominated Transition in Supersonic Boundary Layers on Natural-Laminar-Flow Wing

Kenji Yoshida, Yoshine Ueda, Kenji Yoshida, 2016 .

Transition measurements on the natural laminar flow wing at Mach 2

Akira Nishizawa, Shohei Takagi, Kenji Yoshida, 2001 .

Reduction of the BPF Noise Radiated from an Engine Cooling Fan

Itsuhei Kohri, Yoshihiro Kato, Kenji Yoshida, 2014 .

Particle separation by Iinoya's type gas cyclone

Kenji Yoshida, Hideto Yoshida, Kunihiro Fukui, 2001 .

NUMERICAL STUDY ON TRANSITION PREDICTION METHOD AND EXPERIMENTAL STUDY ON EFFECT OF SUPERSONIC LAMINAR FLOW CONTROL

Kenji Yoshida, Youji Ishida, Kenji Yoshida, 1996 .

Transition Measurements on the Natural Laminar Flow Wing at Mach 2

Akira Nishizawa, Shohei Takagi, Kenji Yoshida, 2001 .

Experimental and numerical analysis of laminar flow control at Mach 1.4

Kenjiro Inagaki, Masayoshi Noguchi, Kenji Yoshida, 1999 .

Studies on strained non-premixed flames affected by flame curvature and preferential diffusion

Toshimi Takagi, Shinichi Kinoshita, Kenji Yoshida, 1996 .

Failure Correlation for Zircaloy-2 Fuel Cladding under High Temperature Transient Conditions

Kenji Yoshida, Akira Tanabe, Susumu Sumida, 1987 .

Modeling of turbulent transport term of interfacial area concentration in gas–liquid two-phase flow

Masanori Naitoh, Kenji Yoshida, Hidetoshi Okada, 2012 .

D-SEND PROJECT FOR LOW SONIC BOOM DESIGN TECHNOLOGY

Kenji Yoshida, Masahisa Honda, .

Summary of CFD Workshop on NEXST-1 flight test

Kenji Yoshida, 憲司吉田, 2007 .

New entrainment rate correlation in annular two-phase flow applicable to wide range of flow condition

Kenji Yoshida, Isao Kataoka, Tsuyoshi Kitahara, 2002 .