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SUMMARYA numerical flutter simulation of a T-tail configuration in the transonic region is presented. A code for aeroelastic simulations based on the multi-block and overset grid concept was developed and has been applied to a T-tail configuration. Flutter simulations are performed at Mach numbers in the range 0.70-0.95, and the obtained results correspond to experimental results. The effect of varying the angle of attack on the flutter boundary is also presented.

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