超静定捆绑火箭传力试验设计方法
Mechanics in Engineering(2017)
Abstract
在综合分析试验产品,边界条件,加载激励,测量可实现性等多方面因素基础上,本文设计了一套超静定捆绑火箭传力试验方法,并通过了地面验证.该设计方法能够有效验证超静定捆绑火箭内力载荷计算的准确性,具有重要的工程指导意义.
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Key words
statically indeterminate,strap-on rocket,force transfer,test design
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