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Aeroelastic Topology Optimization of Wing StructuresGenerational improvement in transport aircraft led to aggressive reductions in noise, emissions, and fuel burn. Technological advances needed across many fronts (aerodynamics, propulsion, alternative fuels, acoustics, structures). Broad structures-centric goals (for wings): stabilize flexibility in minimum-weight wings; and exploit flexibility to reduce wing loading/drag via load redistribution and wing shaping.
Document ID
20200007479
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Bret K Stanford
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 14, 2020
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-18116
Meeting Information
Meeting: Aeroelasticity Branch Peer Review
Location: Hampton, VA
Country: US
Start Date: January 27, 2014
End Date: January 29, 2014
Sponsors: Langley Research Center
Funding Number(s)
WBS: 432938.11.01.07.43.40.08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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