Representation of instantaneous flow velocity field during combustion oscillations in the combustion chamber of a model rocket engine (IMAGE)

Tokyo University of Science

Representation of instantaneous flow velocity field during combustion oscillations in the combustion chamber of a model rocket engine

Caption

This figure shows that large-scale vortex rings are produced from the injector rim during combustion oscillations

Credit

Satomi Shima, Kosuke Nakamura, Hiroshi Gotoda, Yuya Ohmichi, and Shingo Matsuyama

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