Numerical study for the flame deflector design of four-engine liquid rockets
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DOI: 10.1080/19942060.2020.1761453
Abstract: The thermal environment of four-engine liquid rocket exhaust plume impinging on the flame deflector with different impingement and uplift angles is analysed. The supersonic exhaust gas impinging model was established by using the compressible, multi-component,… read more here.
Keywords: angle; deflector; flame deflector; four engine ... See more keywords