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Wind Tunnel Flutter Testing of Composite T-Tail Model of a Transport Aircraft with Fuselage Flexibility

By Raja Samikkannu

Submitted: November 15th 2010Reviewed: March 27th 2011Published: July 27th 2011

DOI: 10.5772/21628

Downloaded: 2455

© 2011 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms of the Creative Commons Attribution-NonCommercial-ShareAlike-3.0 License, which permits use, distribution and reproduction for non-commercial purposes, provided the original is properly cited and derivative works building on this content are distributed under the same license.

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Raja Samikkannu (July 27th 2011). Wind Tunnel Flutter Testing of Composite T-Tail Model of a Transport Aircraft with Fuselage Flexibility, Wind Tunnels and Experimental Fluid Dynamics Research Jorge Colman Lerner, IntechOpen, DOI: 10.5772/21628. Available from:

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