Effect of Aerodynamic Damping Approximations on Aeroelastic Eigensensitivities

نویسندگان

چکیده

Aeroelastic sensitivities for the flutter solution are a crucial component of multi-disciplinary optimization methods employed in modern aircraft design. This paper derives aeroelastic different aerodynamic damping approximations—the p-k method, g method and generalized analysis method—highlighting influence approximation on required derivatives. The derived formulation determination by means direct is verified case two-degree-of-freedom typical section model, where analytical can be analytically obtained. For this an additional namely AGARD 445.6 weakened wing, significant effect shown.

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ژورنال

عنوان ژورنال: Aerospace

سال: 2022

ISSN: ['2226-4310']

DOI: https://doi.org/10.3390/aerospace9030127