NASA NTRS · 19980230613
Experimental Influence Coefficients and Vibration Modes
Abstract
Test results are presented for both symmetrical and antisymmetrical static loading of a wing model mounted on a three-point support system. The first six free-free vibration modes were determined experimentally. A comparison is made of the symmetrical nodal patterns and frequencies with the symmetrical nodal patterns and frequencies calculated from the experimental influence coefficients.
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Weidman, Deene J., Kordes, Eldon E.. 1959-05-01. Experimental Influence Coefficients and Vibration Modes. https://ntrs.nasa.gov/citations/19980230613
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