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Towards Gradient-Based Proprotor Design with VSPAEROGradient-based optimization techniques are an attractive approach to solving multidisciplinary design problems. In this work, the status of gradient-based proprotor optimizations with the VSPAERO code are described.
Document ID
20230014198
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Daniel Ingraham (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
September 29, 2023
Subject Category
Aircraft Design, Testing and Performance
Meeting Information
Meeting: Fall NASA Acoustics Technical Working Group
Location: Cleveland, OH
Country: US
Start Date: October 31, 2023
End Date: November 1, 2023
Sponsors: Glenn Research Center
Funding Number(s)
WBS: 109492.02.03.07.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Multidisciplinary optimization
acoustics
propellers

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