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Experimental investigation and CFD simulation of active damping mechanism for propellant slosh in spacecraft launch systems

机译：航天器发射系统推进剂晃荡主动阻尼机构的实验研究和CFD仿真

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作者
Leuva, Dhawal;
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作者单位

Embry-Riddle Aeronautical University;

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授予单位 Embry-Riddle Aeronautical University;
学科
学位 M.S.A.E.
年度 2011
页码 112 p.
总页数 112
原文格式 PDF
正文语种 eng
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Experimental investigation and CFD simulation of active damping mechanism for propellant slosh in spacecraft launch systems

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