首页 | 本学科首页   官方微博 | 高级检索  
     检索      

整体传递矩阵法求解双转子系统临界转速的改进
引用本文:徐可君,张龙平.整体传递矩阵法求解双转子系统临界转速的改进[J].海军航空工程学院学报,2013,28(2):133-136.
作者姓名:徐可君  张龙平
作者单位:[1]海军航空工程学院青岛校区,山东青岛266041 [2]海军航空工程学院研究生管理大队,山东烟台266001
摘    要:在深入研究现有传统整体传递矩阵算法的基础上,提出了一种改进的整体矩阵方法。该方法有效避免了传统算法中各子结构单元数目相同且需逻辑对齐的要求,不须人为添加虚段或仅在固定位置添加1个或2个虚段,非常有利于编写通用化程序。算例计算表明了该方法的有效性和准确性。

关 键 词:整体传递矩阵法  双转子系统  临界转速  航空发动机

Improvement Method of Dual-Rotor Critical Speed Based on the Whole Transfer Matrix Method
XU Ke-jun and ZHANG Long-ping.Improvement Method of Dual-Rotor Critical Speed Based on the Whole Transfer Matrix Method[J].Journal of Naval Aeronautical Engineering Institute,2013,28(2):133-136.
Authors:XU Ke-jun and ZHANG Long-ping
Institution:(Naval Aeronautical and Astronautical University a. Qingdao Branch, Qingdao Shandong 266041, China; b. Graduate Students'Brigade, Yantai Shandong 264001, China)
Abstract:An improved whole transfer matrix method was proposed in this paper. The advanced method could effectively avoid the requirements that the substructure's element must logic alignment and had the same number in the old algorithm. And the presented method hadno needs to add or only need to add one or two virtual seg- ments in the fixed position. It was very helpful to compile the universal program. The calculated example showed that it was very effective and exact.
Keywords:whole transfer matrix method  dual-rotor system  critical speed  aircraft engine
本文献已被 维普 等数据库收录!
点击此处可从《海军航空工程学院学报》浏览原始摘要信息
点击此处可从《海军航空工程学院学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号