| 书目名称 | The Rotating Beam Problem in Helicopter Dynamics |
| 编辑 | Ranjan Ganguli,Vijay Panchore |
| 视频video | |
| 概述 | Fills a gap in the literature between textbooks on helicopter dynamics and papers published in journals.Illustrates finite element in space and finite element in time, a powerful method for systems go |
| 丛书名称 | Foundations of Engineering Mechanics |
| 图书封面 |  |
| 描述 | .The book addresses computational methods for solving the problem of vibration, response, loads and stability of a helicopter rotor blade modeled as a rotating beam with flap or out-of-plane bending. The focus is on explaining the implementation of the finite element method in the space and time domain for the free vibration, aeroelastic response and stability problems. The use of Floquet analysis for the aeroelastic stability analysis of rotor blades is also shown. The contents of the book will be useful to researchers in aerodynamics and applied mechanics, and will also serve well professionals working in the aerospace industry.. |
| 出版日期 | Book 2018 |
| 关键词 | Finite element method in space; Helicopter flapping blade; Computational method; Finite element method |
| 版次 | 1 |
| doi | https://doi.org/10.1007/978-981-10-6098-4 |
| isbn_softcover | 978-981-13-5566-0 |
| isbn_ebook | 978-981-10-6098-4Series ISSN 1612-1384 Series E-ISSN 1860-6237 |
| issn_series | 1612-1384 |
| copyright | Springer Nature Singapore Pte Ltd. 2018 |
发表于 2025-3-21 19:43:40
