Aeroservoelasticity by Ashish Tewari

Author:Ashish Tewari
Language: eng
Format: epub
Publisher: Springer New York, New York, NY

(4.2)

where is a linear differential operator , and is a functional operator. The solution for the motion coordinates, , requires a simultaneous solution to structural dynamics equations, Eq. (4.1), and unsteady aerodynamic field equations , Eq. (4.2), which could be linear, partial differential equations. The coupled integration of such fluid-structure equations requires iterative solution in the time domain, which is not very amenable to aeroelastic computations.

4.1.1 Traditional Flutter Analysis

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