NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing AircraftThis paper investigates the inertial force effect on nonlinear aeroelasticity of flexible wing aircraft. The geometric are nonlinearity due to rotational and tension stiffening. The effect of large bending deflection will also be investigated. Flutter analysis will be conducted for a truss-braced wing aircraft concept with tension stiffening and inertial force coupling.
Document ID
20160007397
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nguyen, Nhan T. (NASA Ames Research Center Moffett Field, CA United States)
Ting, Eric (SGT, Inc. Moffett Field, CA, United States)
Date Acquired
June 9, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN28796
Report Number: ARC-E-DAA-TN28796
Meeting Information
Meeting: AIAA 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: NNA14AA60C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aeroelasticity

Related Records

There are no records associated with this record.
No Preview Available