Read full paper at: http://www.scirp.org/journal/PaperInformation.aspx?PaperID=52856#.VKs-gMnQrzE Author(s) Kazuhiko Toshimitsu 1 , Shuuto Mikajiri 2 , Ryo Takahashi 3 Affiliation(s) 1 Department of Mechanical Engineering, Oita National College of Technology, Oita, Japan . 2 Mechanical-Environmental System Engineering Major, Oita National College of Technology, Oita, Japan . 3 Department of Computer Science and System Engineering, Kyushu Institute of Technology, Kitakyushu, Japan . ABSTRACT A pulse detonation engine (PDE) is one of candidates of aerospace engines for supersonic cruse. In the paper, a supersonic nozzle ejector is designed to increase thrust of single pulse detonation fo...
Scientific Research Publishing