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Longitudinal Aerodynamic Modeling of the Adaptive Compliant Trailing Edge Flaps on a GIII Airplane and Comparisons to Flight DataDiscuss ACTE aerodynamic modeling efforts and provide comparisons of predictions to flight results for lift and pitching moment increments.

Document ID
20160007779
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Smith, Mark S. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Bui, Trong T. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Garcia, Christian A. (Jacobs Technology, Inc. Edwards AFB, CA, United States)
Cumming, Stephen B. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
June 21, 2016
Publication Date
June 15, 2016
Subject Category
Aircraft Design, Testing And Performance
Aircraft Stability And Control
Aerodynamics
Report/Patent Number
DFRC-E-DAA-TN32815
Meeting Information
Meeting: AIAA Aviation 2016 Conference
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NND08RR01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
aerodynamics
pressure measuments
trailing edge flap

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