Kenichi Rinoie

发表

Experimental Studies of the Flow through an Axial Sudden Expansion with Orifice.

Takuya Ohba, Kenichi Rinoie, Yasuto Sunada, 2000 .

Experimental studies of a 70-degree delta wing with vortex flaps

Kenichi Rinoie, Hirotoshi Fujieda, Toshimi Fujita, 1997 .

AERODYNAMIC CHARACTERISTICS OF ROLLED SST CONFIGURATION WITH LE AND TE FLAPS AT HIGH ANGLES OF ATTACK

Kenichi Rinoie, Toshimi Fujita, Dong-Youn Kwak, 2003 .

Airfoil Stall Suppression Using Rectangular Bubble Burst Control Plate and Sensor Actuators

Yushi Nakamura, Kenichi Rinoie, Yasuto Sunada, 2012 .

Bubble Burst Control Using Smart Structure Sensor Actuators for Stall Suppression

Kenichi Rinoie, Chi Wai Wong, C. Wong, 2009 .

Bubble Burst Control Using Smart Structure Sensor Actuators for Stall Suppression

Kenichi Rinoie, Chi Wai Wong, 2009 .

STUDIES ON THE OPTIMUM PERFORMANCE OF TAPERED VORTEX FLAPS

Kenichi Rinoie, 2000 .

Workload Measurements on Simulated Single Pilot Instrument Flight.

Kenichiro Honda, Kenichi Rinoie, Yasuto Sunada, 2000 .

Pilot Eye Scanning under Actual Single Pilot Instrument Flight.

Kenichi Rinoie, Yasuto Sunada, 2003 .

Lift-to-Drag Ratio Improvement of a Supersonic Transport with Leading-Edge and Trailing-Edge Flaps

Kenichi Rinoie, Dong-Youn Kwak, Katsuhiro Miyata, 2003 .

Studies on vortex flaps with rounded leading edges for supersonic transport configuration

Kenichi Rinoie, Katsuhiro Miyata, Masayoshi Noguchi, 2004 .

Studies on Vortex Flaps Having Different Flap Hinge-Line Positions

Kenichi Rinoie, Dong Youn Kwak, 2001 .

Aerodynamic Characteristics of 4% Cambered-Plate and NACA0012 Airfoil at the Reynolds Numbers Region for Micro Air Vehicles

Kenichi Rinoie, Yasuto Sunada, Asei Tezuka, 2009 .

自律制御機構つき剥離泡崩壊制御板による翼型失速抑制システム;自律制御機構つき剥離泡崩壊制御板による翼型失速抑制システム;Airfoil Stall Suppression by Use of Bubble Burst Control Plate and Autonomous Actuator System

Kenichi Rinoie, Yasuto Sunada, Kenichi Rinoie, 2016 .

Experiments on Vortical Structures Quasi-Periodically Emitted from the Laminar Separation Bubble near Airfoil Stall

Kento Kato, Kenichi Rinoie, Yasuto Sunada, 2019 .

POD Analysis of Two-dimensional Unsteady Flow around I-beam

Taro Imamura, Kenichi Rinoie, Motoshi Harada, 2015 .

Unsteady Measurements in a Separated and Reattaching Flow Formed over a Backward Facing Step.

Kenichi Rinoie, Yasuto Sunada, Yoshihiro Saito, 1998 .

Airfoil stall suppression by use of smart structure sensor actuators for NACA 631-012

Kenichi Rinoie, Chi Wai Wong, 2011 .

Conceptual Design of Biplane with High Aspect Ratio Wings as Next Generation Civil Jet Transport

Taro Imamura, Kenichi Rinoie, Tetsuyuki Masuko, 2016 .

Airfoil Stall Suppression Using Feedback-Controlled Rectangular Bubble-Burst Control Plate

Yushi Nakamura, Kenichi Rinoie, Yasuto Sunada, 2015 .

Experimental Study on the Wing Lift Characteristics of Biplane Micro Air Vehicle

Kenichi Rinoie, Yasuto Sunada, Asei Tezuka, 2009 .

A Low Fidelity Method for Flap Aerodynamic Design of a Cranked-Arrow Wing

Kenichi Rinoie, Dong Youn Kwak, Kentaro Higuchi, 2007 .

Study of Aircraft with Hybrid Laminar Flow Control Based on Exergy Analysis

Kenichi Rinoie, Yoshiki Yanagimoto, K. Rinoie, 2019, AIAA Aviation 2019 Forum.

Experimental Investigation of a Segmented Flap System of a Cranked-Arrow Wing

Kenichi Rinoie, Zhong Lei, Dong-Youn Kwak, 2012 .

Experimental Optimization of Leading-Edge Deflection Angles for an SST Configuration at Low Speed

Kenichi Rinoie, Zhong Lei, Dong-Youn Kwak, 2013 .

Optimum Conceptual Design of Single Engine Turbo-Prop Aircraft

Kenichi Rinoie, Yasuaki Machida, K. Rinoie, 2004 .

Estimation of Take-Off Performance for Supersonic Transport with Leading-Edge Vortex Flaps and Trailing-Edge Flaps

Kenichi Rinoie, Katsuhiro Miyata, K. Rinoie, 2003 .

Roll Characteristics of SST Configuration with Different Outboard Wing Sweepback Angles

Kenichi Rinoie, Yasuto Sunada, Dong-Youn Kwak, 2008 .

Rolling Moment Characteristics of Supersonic Transport Configurations at High Incidence Angles

Kenichi Rinoie, Dong-Youn Kwak, Masayoshi Noguchi, 2006 .

Lift-to-Drag Ratio Improvement on a Supersonic Transport by Leading-Edge Flap at Transonic Regions

Kenichi Rinoie, Dong-Youn Kwak, Katsuhiro Miyata, 2004 .

Benefit and Performance of Various Vortex Flap Configurations

Kenichi Rinoie, 2003 .

Consideration of Future Development of Hybrid Electric Aircraft using Epoch-Era Analysis

Kenichi Rinoie, Tokuta Tanimura, 2021 .

Airfoil Stall Suppression by Use of a Bubble Burst Control Plate

Kenichi Rinoie, Yasuto Sunada, K. Rinoie, 2007 .

Rolling Moment Characteristics at High Alpha on Several Planforms of Cranked Arrow Wing Configuration

Kenichi Rinoie, Dong-Youn Kwak, Hiroyuki Kato, 2009 .

Surface pressure distributions on 4% circular arc airfoil at low Reynolds number

Kenichi Rinoie, Yasuto Sunada, Asei Tezuka, 2008 .

Multi-Point Optimization Study of Hydrogen-Fueled, Low-Boom Supersonic Transport

Kenichi Rinoie, Tatsunori Yuhara, 2012 .

Airfoil Stall Suppression by Use of Rectangular Cross Section Burst Control Plates

Yushi Nakamura, Kenichi Rinoie, Yasuto Sunada, 2012 .

Feasibility Study of Hydrogen Fueled Supersonic Transport

Kenichi Rinoie, Tatsunori Yuhara, 2010 .

Experiments on a 60-Degree Delta Wing with Rounded Leading-Edge Vortex Flaps

Kenichi Rinoie, 2000 .

Experimental Studies of Low Frequency Velocity Disturbances Observed in Short Bubble Formed on Airfoil.

Kenichi Rinoie, Yasuto Sunada, K. Rinoie, 2002 .

Stereoscopic PIV measurements of leading edge separation vortices on a cranked arrow wing

Shigeya Watanabe, Kenichi Rinoie, Dong-Youn Kwak, 2004 .

Laminar airfoil modification attaining optimum drag reduction by use of airfoil morphing

Kenichi Rinoie, Asei Tezuka, K. Rinoie, 2010 .