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Overview: Performance Adaptive Aeroelastic WingAn 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.
Document ID
20180000863
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Hashemi, Kelley (Universities Space Research Association Moffett Field, CA, United States)
Date Acquired
January 31, 2018
Publication Date
November 1, 2017
Subject Category
Aircraft Design, Testing And Performance
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN48403
Report Number: ARC-E-DAA-TN48403
Meeting Information
Meeting: Aerospace Control and Guidance Systems Committee Meeting No. 120
Location: Seattle, WA
Country: United States
Start Date: November 1, 2017
End Date: November 3, 2017
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
CONTRACT_GRANT: NNH15CO48B
Distribution Limits
Public
Copyright
Public Use Permitted.

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