F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver
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Thomas, JP; Custer, CH; Dowell, EH; Hall, KC
Published in: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
December 16, 2010
Presented are flutter-onset trends of the F-16 fighter computed using a harmonic balance version of the NASA OVERFLOW 2 flow solver code. The harmonic technique enables one to model unsteady aerodynamics and aeroelastic response in the frequency domain with reduced computational cost compared to time marching solutions. Computed results compare well to flutter results computed using a separate harmonic balance computational flow solver code developed at Duke University. Select aeroelastic limit cycle oscillation results are also presented. © 2010 by Jeffrey P. Thomas, Chad H. Custer, Earl H. Dowell, and Kenneth C. Hall.
Duke Scholars
Published In
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ISSN
0273-4508
ISBN
9781600867422
Publication Date
December 16, 2010
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Thomas, J. P., Custer, C. H., Dowell, E. H., & Hall, K. C. (2010). F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Thomas, J. P., C. H. Custer, E. H. Dowell, and K. C. Hall. “F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver.” In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2010.
Thomas JP, Custer CH, Dowell EH, Hall KC. F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver. In: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2010.
Thomas, J. P., et al. “F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver.” Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2010.
Thomas JP, Custer CH, Dowell EH, Hall KC. F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2010.
Published In
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ISSN
0273-4508
ISBN
9781600867422
Publication Date
December 16, 2010