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
Ongoing Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
The Technical Cooperating Program Technical Panel 4 (TTCP TP-4) Annual Meeting ; 2014 ; Ottawa, CA
Miscellaneous
No indication
English
Ongoing Fixed Wing Research within the NASA Langley Aeroelasticity Branch (AIAA 2015-2719)
British Library Conference Proceedings | 2015
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