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Dynamic Aeroelasticity Coupling Full Order Geometrically Nonlinear Structures and Full Order Linear Unsteady Aerodynamics - The Joined Wing Case

机译：动态气动弹性耦合全阶几何非线性结构和全阶线性非定常空气动力学-联队机翼案例

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《AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference》|2008年|P.1-32|共32页
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L. Demasi; E. Livne;
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中图分类航空;
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专利

1. Aeroelastic coupling of geometrically nonlinear structures and linear unsteady aerodynamics: Two formulations [J] . L. Demasi, E. Livne Journal of Fluids and Structures . 2009,第5期

机译：几何非线性结构和线性非定常空气动力学的气弹耦合：两种公式
2. On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspect-ratio wings [J] . M. J. Patil, D. H. Hodges Journal of Fluids and Structures . 2004,第7期

机译：空气动力学和结构几何非线性在高纵横比机翼气动弹性行为中的重要性
3. Reduced order nonlinear aeroelasticity of swept composite wings using compressible indicial unsteady aerodynamics [J] . Farsadi Touraj, Rahmanian Mohammad, Kayran Altan Journal of Fluids and Structures . 2020,第期

机译：使用压缩指标不稳定空气动力学减少扫井复合翅膀的订单非线性空气弹性
4. Dynamic Aeroelasticity Coupling Full Order Geometrically Nonlinear Structures and Full Order Linear Unsteady Aerodynamics - The Joined Wing Case [C] . AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference . 2008

机译：动态空气弹性耦合完整阶层几何非线性结构和完整订购线性非稳态空气动力学 - 加入翼壳
5. UNSTEADY AERODYNAMICS IN TIME AND FREQUENCY DOMAINS FOR FINITE-TIME ARBITRARY MOTION OF HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHT (AEROELASTICITY, NONLINEAR PERIODIC SYSTEMS, CASCADE AERO, MODELING, RATIONAL APPROXIMATIONS). [D] . ASGHAR-HESSARI-DINYAVARI, MEHRAN. 1985

机译：悬停和向前飞行中直升机转子叶片有限时任意运动的时间和频率域非定常气动特性（气动弹性，非线性周期系统，级联气动，建模，有理近似）。
6. AEROM: NASA’s Unsteady Aerodynamic and Aeroelastic Reduced-Order Modeling Software [O] . Walter A. Silva -1

机译：AEROM：NASA的非稳态气动和气动弹性降序建模软件
7. Unsteady aerodynamics, reduced-order modelling, and predictive control in linear and nonlinear aeroelasticity with arbitrary kinematics [O] . Simpson Robert J. S. 2016

机译：非定常空气动力学，降阶建模，以及任意运动学的线性和非线性气动弹性的预测控制
8. Nonlinear Large Deflection Theory with Modified Aeroelastic Lifting Line Aerodynamics for a High Aspect Ratio Flexible Wing. [R] . Nguyen, N., Ting, E., Chaparro, D. 2017

机译：高纵横比柔性机翼改进气动弹性提升线空气动力学的非线性大挠度理论。

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