NASA NTRS · 19920074940
A modal model for SCOLE structural dynamics
Abstract
Information on a modal model for the Spacecraft Control Laboratory (SCOLE) is given in viewgraph form. A partial differential equation model covering roll bending, pitch bending, torsion, shear forces, and bending moments is given.
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Joshi, Suresh M.. 1984-01-01. A modal model for SCOLE structural dynamics. https://ntrs.nasa.gov/citations/19920074940
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