Study of linear response identification techniques and reduced-order model generation for a 2D CFD scheme

被引:9
作者
Gaitonde, Ann L. [1 ]
Jones, D. P. [1 ]
机构
[1] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, Avon, England
基金
英国工程与自然科学研究理事会;
关键词
linear pulse responses; reduced-order model; CFD;
D O I
10.1002/fld.1232
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Reduced-Order Models (ROMs) have been the focus of research in various engineering situations, but it is only relatively recently that such techniques have begun to be introduced into the CFD field. The purpose of generating such models is to capture the dominant dynamics of the full set of CFD equations, but at much lower cost. One method that has been successfully implemented in the field of fluid flows is based on the calculation of the linear pulse responses of the CFD scheme coupled with an Eigensystem Realization algorithm (ERA), resulting in a compact aerodynamic model. The key to the models is the identification of the linear responses of the non-linear CFD code. Two different methods have been developed and reported in literature for linear response identification; the first method linearizes the CFD code and the second method uses Volterra theory and the non-linear code. As these methods were developed independently they have not previously been brought together and compared. This paper first explains the subtle, but fundamental differences between the two methods. In addition, a series of test cases are shown to demonstrate the performance and drawbacks of the ROMs derived from the different linear responses. The conclusions of this study provide useful guidance for the implementation of either of the two approaches to obtain the linear responses of an existing CFD code. Copyright (c) 2006 John Wiley & Sons, Ltd.
引用
收藏
页码:1361 / 1402
页数:42
相关论文
共 29 条
[1]  
[Anonymous], 1997, DISSERTATION
[2]  
Aplevich J.D., 2000, ESSENTIALS LINEAR ST
[3]  
BRENNEIS A, 1991, CP507 AGARD
[4]   Reduced-order Modeling of weakly Nonlinear MEMS devices with Taylor-Series expansion and Arnoldi approach [J].
Chen, JH ;
Kang, SM ;
Zou, J ;
Liu, C ;
Schutt-Ainé, JE .
JOURNAL OF MICROELECTROMECHANICAL SYSTEMS, 2004, 13 (03) :441-451
[5]   Accurate numerical integration of state-space models for aeroelastic systems with free play [J].
Conner, MD ;
Virgin, LN ;
Dowell, EH .
AIAA JOURNAL, 1996, 34 (10) :2202-2205
[6]   Modeling of fluid-structure interaction [J].
Dowell, EH ;
Hall, KC .
ANNUAL REVIEW OF FLUID MECHANICS, 2001, 33 :445-490
[7]   Reduced-order models of unsteady viscous flows in turbomachinery using viscous-inviscid coupling [J].
Epureanu, BI ;
Hall, KC ;
Dowell, EH .
JOURNAL OF FLUIDS AND STRUCTURES, 2001, 15 (02) :255-273
[8]   A DUAL-TIME METHOD FOR THE SOLUTION OF THE UNSTEADY EULER EQUATIONS [J].
GAITONDE, AL .
AERONAUTICAL JOURNAL, 1994, 98 (978) :283-291
[9]   Reduced order state-space models from the pulse responses of a linearized CFD scheme [J].
Gaitonde, AL ;
Jones, DP .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2003, 42 (06) :581-606
[10]   A two-dimensional linearized unsteady Euler scheme for pulse response calculations [J].
Gaitonde, AL ;
Jones, DP .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2002, 216 (G2) :89-104