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Aeroelastic Analysis of a Distributed Electric Propulsion Wing
Aeroelastic Tailoring of Transport Wings Including Transonic Flutter Constraints
Aeroservoelastic Optimization under Stochastic Gust Constraints
Aerostructural Level Set Topology Optimization for a Common Research Model Wing
Internal Structural Design of the Common Research Model Wing Box for Aeroelastic Tailoring
Level-Set Topology Optimization with Aeroelastic Constraints
Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces
Sizing and Layout Design of an Aeroelastic Wingbox Through Nested Optimization
Static and Dynamic Aeroelastic Tailoring With Variable Camber Control
Static Loads Testing of a High Aspect Ratio Tow-Steered Wingbox
Status Report on Aeroelasticity in the Vehicle Development for X-57 Maxwell
Whirl Flutter and the Development of the NASA X-57 Maxwell