In the engineering practice the method of static load test is usually used to evaluate the capacity and working status of the existing structure.
工程实践中常常采用静载试验的方法评定既有结构的承载能力及工作状态。
By means of calculating structure strength of the frame and doing static test of the frame quality of strength and rigidity of the frame are discussed in research of static strength loads.
静强度载荷研究：通过机体结构强度计算及全机静力试验，论及静载荷下全机的强度与刚度品质；
Relevant conclusions of structure deformation are gotten through the analysis of deformation curve of static load test of bridge span.
通过对该桥梁跨度静荷载检验变形曲线进行分析，得出了其结构变形的有关结论。
The influence of main structure parameters on static and dynamic characteristics is investigated comprehensively by using orthogonal test design.
应用正交试验设计全面分析结构主要参数对传感器的静、动特性的影响。
First, the static model of off-road vehicle is set up according to its structure and test method and specification for ride comfort.
首先根据越野汽车的结构特点和平顺性试验方法建立越野汽车静态模型；
A method is proposed to detect damages and assess the status of an existing structure from static test data.
基于静态结构识别方法，提出了服役结构损伤探测及状态评估的概率分析方法。
Then, the mathematics model of calculating the surface load and point load in the design of aircraft structure static load test using aircraft surface model is established.
其次结合飞机的曲面外形，建立了飞机结构静力试验设计中的分布式载荷和集中式载荷的演算数学模型。
Based on the superposition principle of linear elasticity, a static model test method — single input, multiple output — was proposed for the static test of such structure.
基于弹性力学的线性叠加原理，针对多点承载桁架式卫星结构的静力试验，提出“单点加载，多点输出”的测试方法。
This paper deals with a structure model test under static load to study the stress characteristics of the structure.
本文介绍北京地铁西单车站一号施工横通道，与正洞导坑交接处开口段结构静载模型试验情况。
During the design of a new aircraft, the suspended static test must be carried out to test whether its structure can satisfy the need of strength specification and CCAR23 air worthiness test.
新飞机研制必须经全机悬空静力试验验证其结构的强度是否满足强度规范和CCAR 23适航条例要求。
During the design of a new aircraft, the suspended static test must be carried out to test whether its structure can satisfy the need of strength specification and CCAR23 air worthiness test.
新飞机研制必须经全机悬空静力试验验证其结构的强度是否满足强度规范和CCAR 23适航条例要求。
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