Effects of injector geometry on scramjet combustor performance

Author:

Chinzei Nobuo1,Komuro Tomoyuki1,Kudou Kenji1,Murakami Atsuo1,Tani Kouichiro1,Masuya Goro1,Wakamatsu Yoshio1

Affiliation:

1. National Aerospace Laboratory, Miyagi 981-15, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

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4. Numerical Simulation of Dual-Mode Scramjet Combustor with Significant Upstream Interaction;International Journal of Manufacturing, Materials, and Mechanical Engineering;2012-07

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