Flutter analysis with structural uncertainty by using CFD-based aerodynamic ROM

Z. Wang, Z. Zhang, D. H. Lee, P. C. Chen, D. D. Liu, Marc Mignolet

Research output: Chapter in Book/Report/Conference proceedingConference contribution

10 Citations (Scopus)

Abstract

This paper presents a novel and efficient methodology for flutter analysis with structural uncertainty in conjunction with an expedient CFD-based aerodynamic reducedorder modeling. The non-parametric structural uncertainty approach allows one rapidly investigate the effects of uncertainty towards to the dynamic system in the case when not enough information about the structural uncertainty is available. With the structural equations represented in the modal space and the baseline structural modal shapes used for all the variations of the structure, one set of aerodynamic reduced-order-models that suit for all the structural variations become feasible and thus significantly reduce the computational expense. Specifically, ARMA models for the generalized aerodynamic forces are developed by using an Euler-based CFD solver. The aeroelastic governing equations are converted into the discrete state-space form, and thereafter can be conveniently linked with the aerodynamic ROMs. The flutter speed is then determined by examining the damping coefficient of the time responses of the modal coordinates. A heavy version of the Goland wing is analyzed as a numerical example to demonstrate the present methodology.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
StatePublished - 2008
Event49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference - Schaumburg, IL, United States
Duration: Apr 7 2008Apr 10 2008

Other

Other49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
CountryUnited States
CitySchaumburg, IL
Period4/7/084/10/08

Fingerprint

ROM
Aerodynamics
Computational fluid dynamics
Flutter (aerodynamics)
Dynamical systems
Damping
Uncertainty

ASJC Scopus subject areas

  • Architecture

Cite this

Wang, Z., Zhang, Z., Lee, D. H., Chen, P. C., Liu, D. D., & Mignolet, M. (2008). Flutter analysis with structural uncertainty by using CFD-based aerodynamic ROM. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Flutter analysis with structural uncertainty by using CFD-based aerodynamic ROM. / Wang, Z.; Zhang, Z.; Lee, D. H.; Chen, P. C.; Liu, D. D.; Mignolet, Marc.

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2008.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Wang, Z, Zhang, Z, Lee, DH, Chen, PC, Liu, DD & Mignolet, M 2008, Flutter analysis with structural uncertainty by using CFD-based aerodynamic ROM. in Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Schaumburg, IL, United States, 4/7/08.
Wang Z, Zhang Z, Lee DH, Chen PC, Liu DD, Mignolet M. Flutter analysis with structural uncertainty by using CFD-based aerodynamic ROM. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2008
Wang, Z. ; Zhang, Z. ; Lee, D. H. ; Chen, P. C. ; Liu, D. D. ; Mignolet, Marc. / Flutter analysis with structural uncertainty by using CFD-based aerodynamic ROM. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2008.
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