NASA NTRS · 19750007567
Optimization of structures to satisfy aeroelastic requirements
Abstract
A method for the optimization of structures to satisfy flutter velocity constraints is presented along with a method for determining the flutter velocity. A method for the optimization of structures to satisfy divergence velocity constraints is included.
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Rudisill, C. S.. 1975-02-01. Optimization of structures to satisfy aeroelastic requirements. https://ntrs.nasa.gov/citations/19750007567
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