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Analytical Flutter Studies of a Subsonic, Actively Controlled, Variable Geometry Wind Tunnel Model. Volume I.

机译：亚音速，主动控制，变几何风洞模型的分析颤振研究。第一卷

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摘要

A structural dynamic system identification was experimentally conducted on a wind tunnel flutter model with active aerodynamic controls. Mass and stiffness parameters were varied on the model to determine an optimum configuration for the wind tunnel tests. (Author)

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作者
Lehman, L.; Stearman, R.;
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年度 1977
页码 1-105
总页数 105
原文格式 PDF
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关键词
Flutter; Aerodynamic control surfaces; Wind tunnel models; Suppression; Aerodynamic configurations; Optimization; Geometry; Stiffness; Mass; Structural response; Vibration;

机译：颤振;空气动力学控制面;风洞模型;抑制;空气动力学配置;优化;几何;刚度;质量;结构响应;振动;

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专利

1. Wind-Tunnel Tests for Active Flutter Control and Closed-Loop Flutter Identification [J] . Huang Rui, Zhao Yonghui, Hu Haiyan AIAA Journal . 2016,第7期

机译：主动式颤振控制和闭环颤振识别的风洞测试
2. Subsonic Wind Tunnel Facility for PIV and blade Flutter Experiments [J] . Kazu TOSHIMITSU, Tetsuaki OGAWA, Satoko MURAKAMI 九州大学工学集報 . 1999,第3期

机译：亚音速风洞设施，用于PIV和叶片颤振实验
3. Design of active flutter suppression and wind-tunnel tests of a wing model involving a control delay [J] . Huang Rui, Qian Wenmin, Hu Haiyan, Journal of Fluids and Structures . 2015,第Null期

机译：具有控制延迟的机翼模型的主动颤振抑制设计和风洞测试
4. Analytical and Experimental Evaluation of Multivariable Stability Margins in Active Flutter Suppression Wind Tunnel Tests [C] . J. K. Berg, K. A. Morgansen, E. Livne, AIAA SciTech Forum and Exposition . 2021

机译：主动扑振抑制风洞试验中多变量稳定性边缘的分析与实验评价
5. Design and Construction of a Wind Tunnel Model with Active Variable Camber Continuous Trailing Edge Flap for Aeroelastic 'In-flight' Shape Optimization Tests [D] . Precup, Nathan 2018

机译：主动可变弯度连续后缘襟翼风洞模型的设计与构建，用于气动弹性“飞行中”形状优化测试
6. Design Manufacturing and Testing of a New Concept for a Morphing Leading Edge using a Subsonic Blow Down Wind Tunnel [O] . David Communier, Franck Le Besnerais, Ruxandra Mihaela Botez, 2019

机译：设计制造和测试使用亚音速放空风洞的变形前沿的新概念
7. MODELING THE BENCHMARK ACTIVE CONTROL TECHNOLOGY WIND- TUNNEL MODEL FOR APPLICATION TO FLUTTER SUPPRESSION [O] . 2008

机译：应用于颤振抑制的基准主动控制技术WIND-TUNNEL模型的建模

Analytical Flutter Studies of a Subsonic, Actively Controlled, Variable Geometry Wind Tunnel Model. Volume I.

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