scholarly journals Numerical Investigation of Wing Section Undergoing Low-Frequency Aeroelastic Limit Cycle Oscillations

AIAA Journal ◽  
2020 ◽  
pp. 1-13
Author(s):  
A. Gross ◽  
H. F. Fasel
2002 ◽  
Vol 8 (5) ◽  
pp. 553-573 ◽  
Author(s):  
Jeonghwan Ko ◽  
Thomas W. Strganac ◽  
John L. Junkins ◽  
Maruthi R. Akella ◽  
Andrew J. Kurdila

The recently derived structured model reference adaptive control (SMRAC) method is considered for the active suppression of limit cycle oscillations for a typical wing section with a structural nonlinearity. The SMRAC method uses the specific structure of the equations of motion governing general mechanical systems. This adaptive control method is implemented and tested in wind tunnel experiments to validate the performance. For comparison, results obtained with adaptive feedback linearization are also presented. It is shown that the derived SMRAC is advantageous in that it suppresses limit cycle oscillations at higher velocities, and also it can rigorously treat actuator saturation a priori.


1998 ◽  
Author(s):  
Guofeng Lin ◽  
Edward Lan ◽  
Jay Brandon

2012 ◽  
Vol 231 (8) ◽  
pp. 3228-3245 ◽  
Author(s):  
Joshua A. Krakos ◽  
Qiqi Wang ◽  
Steven R. Hall ◽  
David L. Darmofal

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