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Spanwise Adaptive WingThis presentation discusses the NASA Armstrong PTERA-SAW flight simulation. The uses of this simulation are to study the aerodynamic effects of moving outer wing panels in flight, develop a flight control system, flight safety analysis, mission planning, flight envelope expansion, and post-flight data analysis.
Document ID
20180004639
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Spivey, David (NASA Armstrong Flight Research Center Edwards, CA, United States)
Suh, Peter (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
August 23, 2018
Publication Date
June 23, 2018
Subject Category
Aircraft Stability And Control
Report/Patent Number
AFRC-E-DAA-TN57916
Report Number: AFRC-E-DAA-TN57916
Meeting Information
Meeting: AIAA Aviation 2018
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 533127.02.17.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
flutter
wing design

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