NASA NTRS · 19720022738
Electromagnetic damper system for ground wind load studies
Abstract
The design, fabrication, and adaptation of a model damper system to the 5.5% aeroelastic model of the Saturn 1B/Skylab launch vehicle are reported. The damper is dynamically calibrated over the desired range of additive damping for model conditions prior to wind tunnel testing.
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Scott, L. P.. 1972-05-01. Electromagnetic damper system for ground wind load studies. https://ntrs.nasa.gov/citations/19720022738
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