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Experimental investigation of inner flow of a throatless diverging rotating detonation engine
Institution:1. Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi, 464-8603, Japan;2. Institute of Materials and System for Sustainability, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi, 464-8603, Japan;3. Department of Mechanical Engineering, Keio University, 3-14-1 Hiyoshi, Kouhoku-ku, Yokohama, Kanagawa, 223-8522, Japan;4. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa, 252-5210, Japan;5. Nets Co Ltd, 2-4 Minami-cho, Sakado, Saitama, 350-0233, Japan;6. School of Mechanical Engineering, Purdue University, 585 Purdue Mall, West Lafayette, IN, 47907, USA;1. Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi, 464-8603, Japan;2. Institute of Materials and Systems for Sustainability, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi, 464-8603, Japan;1. Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi''an 710038, China;2. Institute of Aeroengine, Xi''an Jiaotong University, Xi''an 710049, China;1. School of Aeronautics & Astronautics, Purdue University, West Lafayette, IN 47907, USA;2. School of Mechanical Engineering, Purdue University, West Lafayette, IN 47907, USA;3. Spectral Energies LLC, Beavercreek, OH 45430, USA;4. NASA Glenn Research Center, Cleveland, OH 44135, USA
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