Regression rate and combustion performance investigation on hybrid rocket motor with head-end swirl injection under high geometric swirl number
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DOI: 10.1016/j.ast.2020.105922
Abstract: Abstract It is well known that head-end swirl injection can overcome the key problem of low regression rate and combustion inefficiency in hybrid rocket motor effectively. In this paper, the effect of head-end swirl injection… read more here.
Keywords: swirl injection; swirl; rocket motor; injection ... See more keywords