Daisaku Masaki

发表

NUMERICAL ANALYSIS OF TRANSONIC COMPRESSOR ROTOR FLOW NEAR STALL POINTS

Daisaku Masaki, Shojiro Kaji, 1997 .

Numerical Simulation of a Mixed-flow Compressor under Windmill Conditions

Hideyuki Taguchi, Tetsuya Sato, Daisaku Masaki, 2015 .

System firing tests of a pre-cooled cycle hypersonic turbojet engine

Hiroaki Kobayashi, Kazuhisa Fujita, Shujiro Sawai, 2007 .

Development status of a hypersonic Precooled turbojet engine

Motoyuki Hongoh, Hiroaki Kobayashi, Kazuhisa Fujita, 2009 .

Development study of precooled-cycle hypersonic turbojet engine for flight demonstration

Tetsuya Sato, Hiroaki Kobayashi, Kazuhisa Fujita, 2006 .

Firing Test of a Hypersonic Turbojet Engine Installed on a Flight Test Vehicle

Motoyuki Hongoh, Hiroaki Kobayashi, Tetsuya Sato, 2009 .

Firing Test of Core Engine for Pre-cooled Turbojet Engine

Motoyuki Hongoh, Tetsuya Sato, Kazuhisa Fujita, 2008 .

Preliminary Design Investigation of Electromagnetic Motors for Turbofan-Drive Assist

Takeshi Shinohara, Toshinori Watanabe, Keiichi Okai, 2015 .

Numerical Investigation of Transonic Compressor Flowfields near Stall Part 1 : Examination of Flowfield Transition along the Design Speed Line

Daisaku Masaki, Shojiro Kaji, 1999 .

Development Study of A Precooled Turbojet Engine for Flight Demonstration

Motoyuki Hongoh, Tetsuya Sato, Kazuhisa Fujita, 2008 .

Mach 4 Wind Tunnel Experiment of Hypersonic Pre-Cooled Turbojet Engine

Motoyuki Hongoh, Hiroaki Kobayashi, Hideyuki Taguchi, 2014 .