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NASA NTRS · 19710010664

Optimization under aeroelastic constraints

Abstract

Optimization of aeroelastic constraints for aircraft design using differential equation idealization and finite element approximation

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BibTeXRIS

Ashley, H., Mc Intosh, S. C., Jr., Weatherill, W. H.. 1971-02-01. Optimization under aeroelastic constraints. https://ntrs.nasa.gov/citations/19710010664

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