Aerospace
Technical Paper

Surrogate-model based Optimization Framework for the Structural Design of Helicopter Rotor Blades subject to Dynamics and Failure Criteria

F-0079-2023-18007

5/16/2023

Event
Vertical Flight Society 79th Annual Forum & Technology Display
Authors
Rohin Majeti  German Aerospace Center (DLR)
Franziska Becker  German Aerospace Center (DLR)
Abstract
Content
ABSTRACT

Meta Tags
Topics
Vertical take-off and landing (VTOL)
Propellers and rotors
Optimization
Failure analysis
Calibration
Affiliated or Co-Author
 German Aerospace Center (DLR)
Details
Pages
13
Citation
Majeti, R. and Becker, F., "Surrogate-model based Optimization Framework for the Structural Design of Helicopter Rotor Blades subject to Dynamics and Failure Criteria," Vertical Flight Society 79th Annual Forum & Technology Display, West Palm Beach, Florida, May 16, 2023, .
Additional Details
Publisher
The Vertical Flight Society
Published
5/16/2023
Product Code
F-0079-2023-18007
Content Type
Technical Paper
Language
English