NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Aeroelastic Airworthiness Assesment of the Adaptive Compliant Trailing Edge FlapsTopics treated in this presentation include continuous mold line technologies and linearizing non-linear models in support of airworthiness assessments.
Document ID
20150020459
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Herrera, Claudia Y. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Spivey, Natalie D. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Lung, Shun-Fat (Jacobs Engineering Group, Inc. Edwards AFB, CA, United States)
Ervin, Gregory (FlexSys, Inc. Ann Arbor, MI, United States)
Flick, Peter (Air Force Research Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
November 3, 2015
Publication Date
September 13, 2015
Subject Category
Aircraft Design, Testing And Performance
Air Transportation And Safety
Report/Patent Number
DFRC-E-DAA-TN26639
Report Number: DFRC-E-DAA-TN26639
Meeting Information
Meeting: Society of Flight Test Engineers International Symposium
Location: Lancaster, CA
Country: United States
Start Date: September 14, 2015
End Date: September 17, 2015
Sponsors: Society of Flight Test Engineers
Funding Number(s)
CONTRACT_GRANT: NND08RR01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
ground vibration test
aircraft reliability
flutter analysis
aeroelasticity

Related Records

IDRelationTitle20150020900See AlsoAeroelastic Airworthiness Assesment of the Adaptive Compliant Trailing Edge Flaps20150020900See AlsoAeroelastic Airworthiness Assesment of the Adaptive Compliant Trailing Edge Flaps
No Preview Available