The final test occurred Apr. 21 when the wing and trailing edges were subjected to their limit load of around 2.5g, the highest loads expected to be seen in service.
根据4月21最终试验的结果，机翼和后缘的承受的极限负荷为2.5g左右，而实际最高负荷只能在实际服役的时候才能知道。
For test agents, the CPU speed and memory available will limit the test load.
对测试代理程序而言，CPU速度和可用的记忆体将会限制测试负载。
In this paper, shearing mechanism in the joint core region is analysed from crack to limit state, on the basis of shear test of wrapped steel joint under the monotonic load.
本文根据外包钢节点在单调荷载下的抗剪试验，分析了节点核心区在开裂状态之前及开裂状态到极限状态的抗剪机理，求出了各主要抗剪因素的剪力分配。
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