NASA NTRS · 20200007593
TPSAS-NF1676L-18502-DND
Abstract
1. Aeroelastic tailoring with tow-steered composites 2. Aeroelastic tailoring with functionally-graded metals 3. Wing box topology optimization - Curvilinear rib/spar/stiffener placement - Cellular-based stringer topologies - Optimal topology of lightening holes within ribs/spars - 3D level set methods
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Stanley R Cole. TPSAS-NF1676L-18502-DND. https://ntrs.nasa.gov/citations/20200007593
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