Incorporating Flight Dynamics and Control Criteria in Aircraft Design Optimization
The NASA Performance Adaptive Aeroelastic Wing (PAAW) project goals include significant reductions in fuel burn, emissions, and noise via efficient aeroelastic design and improvements in propulsion systems. As modern transport airplane designs become increasingly lightweight and incorporate high asp...
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Virginia Tech
2021
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| Online Access: | http://hdl.handle.net/10919/104967 |