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超声速边界层/混合层组合流动的稳定性分析 总被引:1,自引:0,他引:1
利用可压缩线性稳定性理论研究了超声速混合层考虑壁面影响流动时的失稳特性. 基本流场选取了具有不同速度特征的2 股均匀来流,进入存在上下壁面的流道中. 混合层与边界层的距离为1~3 个边界层厚度,其中壁面取为绝热壁. 分析了该流动在超声速情况下的稳定性特征,同时还讨论了不同波角下的三维扰动波的演化特点,并与二维扰动波进行了比较和分析. 研究结果表明,在此流动情况下,边界层流动和混合层流动的稳定性特征同时存在,并互有影响,其流动稳定性特征既有别于单纯的平板边界层,也有别于单纯的平面混合层,呈现出了新的稳定性特征. 相似文献
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The geometries of Mg n Ni 2(n = 1-6) clusters are studied by using the hybrid density functional theory(B3LYP) with LANL2DZ basis sets.For the ground-state structures of Mg n Ni 2 clusters,the stabilities and the electronic properties are investigated.The results show that the groundstate structures and symmetries of Mg clusters change greatly due to the Ni atoms.The average binding energies have a growing tendency while the energy gaps have a declining tendency.In addition,the ionization energies exhibit an odd-even oscillation feature.We also conclude that n = 3,5 are the magic numbers of the Mg n Ni 2 clusters.The Mg 3 Ni 2 and Mg 5 Ni 2 clusters are more stable than neighbouring clusters,and the Mg 4 Ni 2 cluster exhibits a higher chemical activity. 相似文献
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基于Lyapunov稳定理论研究非周期采样控制系统的稳定性问题.首先,通过充分利用系统的状态信息,构建出新的增广型Lyapunov-Krasovskii泛函,并引入零等式来放宽泛函的正定条件;其次,在对泛函导数进行界定时,应用自由矩阵积分不等式方法估计泛函导数中的积分项,得到了更小保守性的稳定性判据.最后,借助一个经典... 相似文献
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Employing the density functional theory, we investigate the lowest-energy geometric, the stable and the electronic properties of Agn-1Y (n=2-10) clusters in this paper. The structural optimization and the frequency analysis are performed at the B3LYP/LANL2DZ level. Meanwhile, the differences in geometry, stability and electronic properties between Agn and Agn-1Y (n=2-10) clusters are also studied. The results show that for the doping of the yttrium atoms, the structures and the average binding lengths of the Agn clusters are greatly changed. In addition, the thermodynamic stabilities of the Agn clusters are enhanced generally with the doping of the Y atoms. In addition, the chemical stabilities of the Agn-1Y clusters are still improved compared with that of the three-dimensional Agn clusters. 相似文献
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在新型火箭研制阶段,如何确定起飞段运载火箭的声源以及发动机的喷流噪声十分重要.该文对试车台上某型液体火箭发动机单机试车时发动机产生的喷流噪声和发动机上方目标声场进行了多次测量,并基于统计能量分析方法建立了该发动机的声振分析模型.以试验和计算相结合的方法对目标声场进行仿真计算,并和试车台上目标声场测试结果进行了对比分析,所得结论对获得箭体关键部位的噪声频谱具有重要作用. 相似文献