NASA NTRS · 19750035997
Vibration and flutter analysis of reusable surface insulation panels
Abstract
A study has been conducted of the aeroelastic behavior of heat shield panels for the thermal protection system of the space shuttle. Questions of structural and aerodynamic modeling are considered along with the analysis of a single isotropic tile and an isotropic main substructure. Representative flutter results are presented, taking into account a rigid and a flexible metallic substructure.
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Dowell, E. H.. 1975-01-01. Vibration and flutter analysis of reusable surface insulation panels. https://ntrs.nasa.gov/citations/19750035997
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