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Viscous and Aeroelastic Effects on Wind Turbine Blades. The VISCEL Project. Part Ⅱ: Aeroelastic Stability Investigations

机译:风力涡轮机叶片的粘性和气弹效应。 VISCEL项目。第二部分:气动弹性稳定性研究

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The recent introduction of ever larger wind turbines poses new challenges with regard to understanding the mechanisms of unsteady flow-structure interaction. An important aspect of the problem is the aeroelastic stability of the wind turbine blades, especially in the case of combined flap/lead-lag vibrationsin the stall regime. Given the limited experimental information available in this field, the use of CFD techniques and state-of-the-art viscous flow solvers provides an invaluable alternative towards the identification of the underlying physics and the development and validation of sound engineering-type aeroelastic models. Navier-Stokes-based aeroelastic stability analysis of individual blade sections subjected to combined pitch/flap or flap/lead-lag motion has been attempted by the present consortium in the framework of the concluded VISCEL JOR3-CT98-0208 Joule Ⅲ project.
机译:最近引入的越来越大的风力涡轮机在理解不稳定的流固耦合机制方面提出了新的挑战。该问题的重要方面是风力涡轮机叶片的气动弹性稳定性,尤其是在失速状态下襟翼/超前-滞后振动组合的情况下。鉴于该领域中可用的实验信息有限,使用CFD技术和最新的粘滞流动求解器可以为鉴定基础物理以及开发和验证声音工程类型的气动弹性模型提供宝贵的替代方案。本财团已在已完成的VISCEL JOR3-CT98-0208 JouleⅢ项目的框架内尝试对基于桨叶/襟翼或襟翼/超前-滞后运动的单个叶片截面进行基于Navier-Stokes的气动弹性稳定性分析。

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