Structural Optimization and Aeroelastic Analysis of a Composite T-Tail Configuration

Li Liang; Sun Qin

doi:10.4028/www.scientific.net/AMR.466-467.1125

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 466-467Structural Optimization and Aeroelastic Analysis...

Structural Optimization and Aeroelastic Analysis of a Composite T-Tail Configuration

Abstract:

In this paper, a composite T-tail model is developed, including structural finite element model and aeroelastic model, and then structural optimization and aeroelastic analysis are made. Through two steps of structural optimization, and aeroelastic analysis, some valuable conclusions are achieved, which are useful for future composite T-tail design.

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Periodical:

Advanced Materials Research (Volumes 466-467)

Pages:

1125-1128

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.466-467.1125

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Online since:

February 2012

Authors:

Li Liang, Sun Qin

Keywords:

Aeroelastic Analysis, Composite T-Tail, Structural Optimization

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References

[1] G.R. Andersen, D.L. Cowan, and D.J. Piatak. Aeroelatic modeling, Analysis and testing of a morphing wing structure, AIAA 2007-1734.

DOI: 10.2514/6.2007-1734

Google Scholar

[2] M.Z. Tao. Modern Structural Design of Aircraft. Northwestern Polytechnic University Press, (2001).

Google Scholar

[3] B.S. Liu, C. Huang. Patran from Introduction to Proficiency. Chinese Water and Power Press, (2003).

Google Scholar

[4] N.B. Yang, Y.N. Zhang. Composite Structure Design of Aircraft. Beijing Aviation Industry Press, (2002).

Google Scholar

[5] W.P. Jcnnings, M.A. Berry. The Flutter Analysis of T-tails, AIAA 75-759.

Google Scholar

[6] A. Attorni, L. Cavagna, G. Quaranta. Aircraft T-tail Flutter Predictions Using Computational Fluid Dynamics, Journal of Fluids and Structures, 2010. 11.

DOI: 10.1016/j.jfluidstructs.2010.11.003

Google Scholar