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NASA NTRS · 19830013232

Aeroelastic instability stoppers for wind tunnel models

Abstract

A mechanism for constraining models or sections thereof, was wind tunnel tested, deployed at the onset of aeroelastic instability, to forestall destructive vibrations in the model is described. The mechanism includes a pair of arms pivoted to the tunnel wall and straddling the model. Rollers on the ends of the arms contact the model, and are pulled together against the model by a spring stretched between the arms. An actuator mechanism swings the arms into place and back as desired.

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BibTeXRIS

Doggett, R. V., Jr., Ricketts, R. H.. 1981-06-17. Aeroelastic instability stoppers for wind tunnel models. https://ntrs.nasa.gov/citations/19830013232

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