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Analysis of a Fluttering Delta Wing with Large Deformation at Low Subsonic Speeds

机译：低亚音速速度变形的絮凝三角翼分析

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Atsushi Hashimoto; Yasuyuki Furuta; Naoto Yagi; Yoshiaki Nakamura;
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年度 2007
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1. Flutter analysis of an articulated high aspect ratio wing in subsonic airflow [J] . A.V. Balakrishnan, Amjad M. Tuffaha, Iylene Patino, Journal of the Franklin Institute . 2014,第8期

机译：亚音速气流中铰接式高纵横比机翼的颤振分析
2. Aeroelastic Analysis of a Composite Material Delta Wing in Low Subsonic Flow [J] . Kedar S. Sapkal, Peter J. Attar AIAA Journal . 2012,第1期

机译：低亚音速流中复合材料三角翼的气动弹性分析
3. Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing's parameters on flutter speed [J] . Thi Tuyet Nhung Le, Chi-Cong Nguyen, Hoang Nam Vang International Journal of Mechanical Engineering and Applications . 2015,第1a3期

机译：低速风洞中NACA0012机翼模型的空气弹性台架试验设计：机翼参数对扑扑速度的影响
4. Analysis of Vortex Flow Phenomena on Generic Delta Wing Planforms at Subsonic Speeds [C] . Stefan Pfnur, Jonathan Pfluger, Christian Breitsamter STAB/DGLR Symposium . 2020

机译：血液速度通用Delta Wing Planforms涡流流动现象分析
5. Formulation of a structural model for flutter analysis of low aspect ratio composite aircraft wings. [D] . Seitz, Timothy J. 1992

机译：为低长宽比复合材料飞机机翼的颤振分析建立结构模型。
6. On fluttering modes for aircraft wing model in subsonic air flow [O] . Marianna A. Shubov -1

机译：亚音速气流中机翼模型的颤振模式
7. Some low-speed flutter characteristics of simple low-aspect-ratio delta wing models [O] . Soistmann David L., Doggett Robert V. Jr. 1989

机译：简单低纵横比三角翼模型的一些低速颤振特性
8. Possio's Subsonic Derivative Theory and its Application to Flexural-Torsional Wing Flutter PART I Possio's Derivative Theory for an Infinite Aerofoil Moving at Subsonic Speeds PART II Influence of Compressibility on the Flexural-Torsional Flutter of a Tapered Cantilever Wing Moving at Subsonic Speed [R] . R. A. FRAZER, R. A. FRAZER 1951

机译：possio的亚音速导数理论及其在弯扭翼展中的应用第一部分possio的无限翼型在亚音速速度下的导数理论第二部分压缩性对锥形悬臂梁弯曲 - 扭转颤振的影响以亚音速运动

Analysis of a Fluttering Delta Wing with Large Deformation at Low Subsonic Speeds

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