| 书目名称 | Progress in Computational Flow-Structure Interaction |
| 副标题 | Results of the Proje |
| 编辑 | Werner Haase,Vittorio Selmin,Bengt Winzell |
| 视频video | |
| 概述 | State of the art in computational fluid dynamics and nonlinear aeroelasticity.Includes supplementary material: |
| 丛书名称 | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
| 图书封面 |  |
| 描述 | Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever increasing aircraft size and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads discipl |
| 出版日期 | Conference proceedings 2003 |
| 关键词 | CFD; Fluid-Structure Interaction; computational fluid dynamics; nonlinear aeroelastity; unsteady flow; un |
| 版次 | 1 |
| doi | https://doi.org/10.1007/978-3-540-45489-2 |
| isbn_softcover | 978-3-642-07868-2 |
| isbn_ebook | 978-3-540-45489-2Series ISSN 1612-2909 Series E-ISSN 1860-0824 |
| issn_series | 1612-2909 |
| copyright | Springer-Verlag Berlin Heidelberg 2003 |
发表于 2025-3-21 19:51:24
