NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Evaluation of the Hinge Moment and Normal Force Aerodynamic Loads from a Seamless Adaptive Compliant Trailing Edge Flap in FlightThis presentation describes the interface hinge moments loads collected during the ACTE flights.
Document ID
20160000937
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Miller, Eric J. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Cruz, Josue (NASA Armstrong Flight Research Center Edwards, CA, United States)
Lung, Shun-Fat (NASA Armstrong Flight Research Center Edwards, CA, United States)
Sridhar, Kota (FlexSys, Inc. Ann Arbor, MI, United States)
Ervin, Gregory (FlexSys, Inc. Ann Arbor, MI, United States)
Lu, Kerr-Jia (FlexSys, Inc. Ann Arbor, MI, United States)
Flick, Pete (Air Force Research Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
January 19, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AFRC-E-DAA-TN28829
Report Number: AFRC-E-DAA-TN28829
Meeting Information
Meeting: SciTech 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NND08RR01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Adaptive Compliant Trailing Edge
Hinge Moment Loads
Trailing Edge Flap Loads

Related Records

IDRelationTitle20160000870See AlsoEvaluation of the Hinge Moment and Normal Force Aerodynamic Loads from a Seamless Adaptive Compliant Trailing Edge Flap in Flight
No Preview Available