超静定捆绑火箭传力试验设计方法

摘要

Based on the comprehensive analysis of the test products, the loading force, the boundary conditions, the measurement practicability, the force transfer test for statically indeterminate rockets is designed, and validated by tests. The test design method can be used to verify the correctness of the calculation of the internal force of the statically indeterminate rocket effectively.%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.