Flutter Condition Estimation for 3-D Cantilever Plate Using Fully Coupled Fluid – Structure Interaction
Flutter Condition Estimation for 3-D Cantilever Plate Using Fully Coupled Fluid – Structure Interaction

Hayder Sabah Abd Al-Amir; Mauwafak Ali Tawfik; Mohammed Idris Abu-Tabikh

Volume 32, Issue 12 , November 2014, , Page 3038-3055

https://doi.org/10.30684/etj.32.12A.14

Abstract
  The aeroelastic responses and the flutter condition of 3-D flexible cantilever plate were estimated by developed fully coupled fluid-structure interaction(FSI) approach. The plate model ...  Read More ...
Flutter Estimation for Low Speed Aircraft Wing Using Fully Coupled Fluid – Structure Interaction
Flutter Estimation for Low Speed Aircraft Wing Using Fully Coupled Fluid – Structure Interaction

Mauwafak Ali Tewfik; Mohammed Idris Abu-Tabikh; Hayder Sabah Abd Al-Amir

Volume 31, Issue 16 , September 2013, , Page 3203-3215

https://doi.org/10.30684/etj.31.16A.15

Abstract
  The aero elastic responses and the flutter condition of 3-D flexible aircraft wing were estimated by developed fully coupled fluid-structure interaction approach. The actual wing in ...  Read More ...
Control on 3-D Fixable Wing Flutter Using an Adaptive Neural Controller
Control on 3-D Fixable Wing Flutter Using an Adaptive Neural Controller

Mauwafak Ali Tawfik; Mohammed Idris Abu-Tabikh; Hayder Sabah Abd Al-Amir

Volume 30, Issue 16 , September 2012, , Page 2858-2874

https://doi.org/10.30684/etj.30.16.9

Abstract
  An adaptive neural controller to control on flutter in 3-D flexible wing is proposed. The aeroelastic model was based on the coupling between structure-of the equivalent plate (wing) ...  Read More ...