A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow
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, Conference
Thomas, JP; Hall, KC; Dowell, EH
Published in: 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
January 1, 2003
Presented is a frequency-domain harmonic-balance (HB) computational fluid dynamic (CFD) approach for modeling flutter onset and limit cycle oscillation (LCO) behavior of viscous transonic aeroelastic wing configurations. The AGARD 445.6 transonic wing configuration is studied and results are compared to a recent inviscid analysis for a supersonic Mach number flow condition. © 2003 by Jeffrey P. Thomas, Kenneth C. Hall, and Earl H. Dowell. Published by the American Institute of Aeronautics and Astronautics, Inc.
Duke Scholars
Published In
44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
DOI
Publication Date
January 1, 2003
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Thomas, J. P., Hall, K. C., & Dowell, E. H. (2003). A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow. In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. https://doi.org/10.2514/6.2003-1924
Thomas, J. P., K. C. Hall, and E. H. Dowell. “A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2003. https://doi.org/10.2514/6.2003-1924.
Thomas JP, Hall KC, Dowell EH. A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow. In: 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2003.
Thomas, J. P., et al. “A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow.” 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2003. Scopus, doi:10.2514/6.2003-1924.
Thomas JP, Hall KC, Dowell EH. A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow. 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2003.
Published In
44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
DOI
Publication Date
January 1, 2003