Nonlinear aeroelasticity

Author(s):  
Edward F. Crawley ◽  
Howard C. Curtiss ◽  
David A. Peters ◽  
Robert H. Scanlan ◽  
Fernando Sisto
2018 ◽  
Vol 18 (06) ◽  
pp. 1871006 ◽  
Author(s):  
Yaobin Niu ◽  
Zhongwei Wang

In this paper, a new modified harmonic balance method is presented for the nonlinear aeroelastic analysis of two degree-of-freedom airfoils. Using this method, the nonlinear problem is first translated into a minimization problem, and the Particle Swarm Optimization which has high calculation efficiency is adopted to solve the problem. The proposed method is used to solve the nonlinear aeroelastic behavior of supersonic airfoil, with the unsteady aerodynamic load evaluated by the piston theory. Three examples of nonlinear aeroelasticity with significantly different coefficients are prepared, in which the frequencies and amplitudes of the limit cycles are obtained. The results show that the present current method is computationally more efficient.


Author(s):  
Rocco Bombardieri ◽  
Rauno Cavallaro ◽  
Jorge Luis Sáez de Teresa ◽  
Moti Karpel

2019 ◽  
Vol 54 (5) ◽  
pp. 740-740
Author(s):  
Hairun Xie ◽  
Yadong Wu ◽  
Hua Ouyang ◽  
Anjenq Wang

2014 ◽  
Vol 977 ◽  
pp. 418-422
Author(s):  
Rui Li ◽  
Chang Hong Tang

the origins and characteristics of linear and nonlinear aeroelasticity are analyzed.And the deforming mesh , fluid-structure coupling schemes, the design method of aerodynamic module and structure module interface are also analyzed. their advantages and disadvantages are Pointed out. Finally, several recommendations are given for the development orientation of aeroelasticity in the future.


2004 ◽  
Vol 50 (4) ◽  
pp. 221-235 ◽  
Author(s):  
Azzeddine Soulaïmani ◽  
Amine Ben Haj Ali ◽  
Zhengkun Feng

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