Please use this identifier to cite or link to this item:
|Title:||Identification of a Hammerstein model for wing flutter analysis using CFD data and correlation method||Authors:||Lum, K.-Y.
|Issue Date:||2010||Citation:||Lum, K.-Y.,Lai, K.L. (2010). Identification of a Hammerstein model for wing flutter analysis using CFD data and correlation method. Proceedings of the 2010 American Control Conference, ACC 2010 : 1314-1319. ScholarBank@NUS Repository.||Abstract:||A correlation approach for the identification of a Hammerstein model of unsteady aerodynamics using CFD data is presented. The main idea is to use correlation functions of the input-output processes as data for the identification problem. It is shown in a numerical example of the AGARD 445.6 wing that the proposed method can more accurately approximate the linear aerodynamic response, which is needed for a first-order prediction of wing flutter boundaries. © 2010 AACC.||Source Title:||Proceedings of the 2010 American Control Conference, ACC 2010||URI:||http://scholarbank.nus.edu.sg/handle/10635/111590||ISBN:||9781424474264|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Mar 6, 2021
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.