Tatsunori Yuhara

Studies on Wingtip Geometries by Optimum Spanwise Lift Distribution Design Method

Kenichi Rinoie, Yuki Oda, Tatsunori Yuhara, 2017 .

Drag/Weight Reduction Using Split-Tip Winglet for TRA2012A Model

Wataru Yamazaki, Tatsunori Yuhara, Soichiro Tabata, 2020, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES.

Conceptual Design Study on LH 2 Supersonic Transport for the 2030-2035 time frame

Kenichi Rinoie, Tatsunori Yuhara, K. Rinoie, 2012 .

2A1-H07 Development of airplane type UAV capable of hovering vertically to drop object(Aerial Robot and Mechatronics(1))

Taro Imamura, Tatsunori Yuhara, Kohei Miyazono, 2012 .

Airport Noise Estimation within the Conceptual Design Study on LH2-Fueled Supersonic Transport

Yoshikazu Makino, Kenichi Rinoie, Tatsunori Yuhara, 2017 .

Conceptual Design Study on Liquid Hydrogen-Fueled Supersonic Transport Considering Environmental Impacts

Yoshikazu Makino, Kenichi Rinoie, Tatsunori Yuhara, 2016 .

Multi-disciplinary Optimization of Split-Tip Winglet and Extraction of Design Knowledge by Dimension Reduction Technology

Wataru Yamazaki, Tatsunori Yuhara, Soichiro Tabata, 2021, The Proceedings of Conference of Hokuriku-Shinetsu Branch.

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

Kenichi Rinoie, Tatsunori Yuhara, 2012 .

Feasibility Study of Hydrogen Fueled Supersonic Transport

Kenichi Rinoie, Tatsunori Yuhara, 2010 .