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Ongoing Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch 1. Aeroelastic tailoring with tow-steered composites
2. Aeroelastic tailoring with functionally-graded metals
3. Wing box topology optimization
- Curvilinear rib/spar/stiffener placement
- Cellular-based stringer topologies
- Optimal topology of lightening holes within ribs/spars
- 3D level set methods
Document ID
20200007593
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Stanley R Cole
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 14, 2020
Subject Category
Aerodynamics
Report/Patent Number
Report Number: NF1676L-18502
NF1676L-18502
Meeting Information
Meeting: The Technical Cooperating Program Technical Panel 4 (TTCP TP-4) Annual Meeting
Location: Ottawa
Country: CA
Start Date: March 24, 2014
End Date: March 28, 2014
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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