Motoyuki Hongoh

Study on variable-shape supersonic inlets and missiles with MRD device

K. Okai, Y. Maru, T. Kojima, 2007 .

Development status of the hypersonic turbojet engine for Mach 5 flight in JAXA

Motoyuki Hongoh, Hiroaki Kobayashi, Hideyuki Taguchi, 2011 .