Surrogate-model based Optimization Framework for the Structural Design of Helicopter Rotor Blades subject to Dynamics and Failure Criteria
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- 13 pages
- SKU # : F-0079-2023-18007 Aircraft Design
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Surrogate-model based Optimization Framework for the Structural Design of Helicopter Rotor Blades subject to Dynamics and Failure Criteria
Authors / Details:Rohin Kumar Majeti, Franziska Becker, German Aerospace Center (DLR)
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