An overview of recent aeroelasitc wing-shaping work at the NASA Ames Research Center is presented. The highlight focuses on activity related to the Performance Adaptive Aeroelastic Wing concept and related Variable Camber Continuous Trailing Edge Flap actuation system. Topics covered include drag-reducing configurations and online algorithms, gust and maneuver load techniques, and wind tunnel demonstrations.
Overview: Performance Adaptive Aeroelastic Wing
Aerospace Control and Guidance Systems Committee Meeting No. 120 ; 2017 ; Seattle, WA, United States
2017-11-01
Miscellaneous
No indication
English
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