
doi: 10.2514/3.12841
The purpose is to outline an approach to the approximation of the kernel function. To this end, the kernel function has been approximated with a portion of the integrand in the kernel replaced with a simple curve fit. This curve fit employs functions that render the integrand readily integrable. The accuracy of this approximation could be questioned, but as shown in example calculations, the presented method compares well to the generally accepted asymptotic results.
planar wing, General aerodynamics and subsonic flows, harmonic vibrations
planar wing, General aerodynamics and subsonic flows, harmonic vibrations
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