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Flexible Wing Designs with Sensor Control Feedback for Demonstration on the X-56A (MUTT)Presenting an overview of the research DFRC is planning within the Subsonic Fixed Wing (SFW) Light Weight Airframes and Propulsion. Describ ing our TRL maturation and new research going forward using the X-56A as a validation testbed.
Document ID
20120011870
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Ginn, Starr (NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 26, 2013
Publication Date
March 13, 2012
Subject Category
Aerodynamics
Report/Patent Number
DFRC-E-DAA-TN4938
Report Number: DFRC-E-DAA-TN4938
Meeting Information
Meeting: Fundamental Aero Program Technical Conference
Location: Cleveland, OH
Country: United States
Start Date: March 13, 2012
End Date: March 15, 2012
Funding Number(s)
WBS: WBS 432938.08.01.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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