Under higher temperatures the charge within a warhead will be subjected to physical and chemical changes, which will influence the security of the warhead launching process. In this paper the problem is studied adopti...Under higher temperatures the charge within a warhead will be subjected to physical and chemical changes, which will influence the security of the warhead launching process. In this paper the problem is studied adopting finite difference method for the case of a rocket powered missile. Temperature distribution tables are given through quadrature experiments, and the results fit the actual measured values very well. The results also show that to ensure the launching security of rocket powered missiles having warhead charge critical temperature close to about 60?℃, the designer can select appropriate heat insulation structural parameters.展开更多
随着风电大规模并网,其波动性、间歇性及时空相关性对可用输电能力(available transfer capability,ATC)计算带来极大挑战,建立考虑风速时空相关性的基于直流潮流的含风电场系统可用输电能力计算模型。同时考虑风速时空相关性与负荷波...随着风电大规模并网,其波动性、间歇性及时空相关性对可用输电能力(available transfer capability,ATC)计算带来极大挑战,建立考虑风速时空相关性的基于直流潮流的含风电场系统可用输电能力计算模型。同时考虑风速时空相关性与负荷波动性对系统潮流分布的影响,并采用交替方向乘子法(alternating direction method of multipliers,ADMM)对ATC模型进行优化求解,以提高计算速度,实现系统ATC的快速计算。以IEEE-9、IEEE-39、IEEE-118测试系统进行仿真,验证该算法的准确性和有效性。展开更多
文摘Under higher temperatures the charge within a warhead will be subjected to physical and chemical changes, which will influence the security of the warhead launching process. In this paper the problem is studied adopting finite difference method for the case of a rocket powered missile. Temperature distribution tables are given through quadrature experiments, and the results fit the actual measured values very well. The results also show that to ensure the launching security of rocket powered missiles having warhead charge critical temperature close to about 60?℃, the designer can select appropriate heat insulation structural parameters.
文摘随着风电大规模并网,其波动性、间歇性及时空相关性对可用输电能力(available transfer capability,ATC)计算带来极大挑战,建立考虑风速时空相关性的基于直流潮流的含风电场系统可用输电能力计算模型。同时考虑风速时空相关性与负荷波动性对系统潮流分布的影响,并采用交替方向乘子法(alternating direction method of multipliers,ADMM)对ATC模型进行优化求解,以提高计算速度,实现系统ATC的快速计算。以IEEE-9、IEEE-39、IEEE-118测试系统进行仿真,验证该算法的准确性和有效性。
