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Using Loft: An Automated Parametric Mesh Generator for Stiffened Shell Aerospace Vehicles
Document ID
20230015266
Acquisition Source
Langley Research Center
Document Type
Presentation
External Source(s)
LAR-18704-1
Authors
Lloyd B Eldred (Langley Research Center Hampton, Virginia, United States)
Date Acquired
October 20, 2023
Subject Category
Structural Mechanics
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 725017.02.07.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Loft
FEA
mesh
parametric

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